Explore: Inviscid Flow
Discover books, insights, and more — all in one place.
Learn more about Inviscid Flow with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “inviscid-flow”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Ship resistance and flow
By Lars Larsson
“Ship resistance and flow” Metadata:
- Title: Ship resistance and flow
- Author: Lars Larsson
- Language: English
- Number of Pages: Median: 230
- Publisher: ➤ The Society of Naval Architects and Marine Engineers - Society of Naval Architects and Marine Engineers
- Publish Date: 2010
- Publish Location: Jersey City, N.J
“Ship resistance and flow” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Hydrodynamics - Mathematics - Ship resistance - Ships - Hulls (Naval architecture) - Navires - Résistance - Mathématiques - Écoulement non visqueux - Écoulement visqueux - Hydrodynamique - Military & Naval Science - Law, Politics & Government - Naval Architecture
Edition Identifiers:
- The Open Library ID: OL24552985M
- Online Computer Library Center (OCLC) ID: 633140570 - 746854818
- Library of Congress Control Number (LCCN): 2010020298
- All ISBNs: 0939773767 - 9780939773763
Access and General Info:
- First Year Published: 2010
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
Find Ship resistance and flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Efficient gradient-based shape optimization methodology using inviscid/viscous CFD
By Oktay Baysal
“Efficient gradient-based shape optimization methodology using inviscid/viscous CFD” Metadata:
- Title: ➤ Efficient gradient-based shape optimization methodology using inviscid/viscous CFD
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Norfolk, Va
“Efficient gradient-based shape optimization methodology using inviscid/viscous CFD” Subjects and Themes:
- Subjects: ➤ Alternating direction implicit methods - Computational fluid dynamics - Flow equations - Gradients - Inviscid flow - Navier-Stokes equation - Optimization - Shapes - Three dimensional flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17126493M - OL17837326M - OL15505689M - OL18121650M
- Online Computer Library Center (OCLC) ID: 40216986
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Efficient gradient-based shape optimization methodology using inviscid/viscous CFD at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
By Ing Chuang
“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Metadata:
- Title: ➤ CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
- Author: Ing Chuang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Computational fluid dynamics - Turbojet engines - Engine design - Nozzle geometry - Hypersonic flight - Nozzle thrust coefficients - Flow distribution - Ramjet engines - Nozzle walls
Edition Identifiers:
- The Open Library ID: OL18120912M - OL17593566M - OL15503241M - OL17134628M
- Online Computer Library Center (OCLC) ID: 42555294
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Solution-adaptive Cartesian cell approach for viscous and inviscid flows
By William J. Coirier
“Solution-adaptive Cartesian cell approach for viscous and inviscid flows” Metadata:
- Title: ➤ Solution-adaptive Cartesian cell approach for viscous and inviscid flows
- Author: William J. Coirier
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1996
- Publish Location: ➤ Washington, DC - Springfield, Va
“Solution-adaptive Cartesian cell approach for viscous and inviscid flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Euler equations of motion - Finite volume method - Grid generation (Mathematics) - Inviscid flow - Navier-Stokes equation - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17129383M - OL15538681M - OL18131753M - OL17592998M
- Online Computer Library Center (OCLC) ID: 40989514
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Solution-adaptive Cartesian cell approach for viscous and inviscid flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
By E. Carson Yates
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Metadata:
- Title: ➤ Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Inviscid flow - Viscous flow - Integral equations - Unsteady aerodynamics - Transonic flow - Computer aided design - Supersonics
Edition Identifiers:
- The Open Library ID: OL20650523M - OL17630478M - OL16131061M - OL18246750M
- Online Computer Library Center (OCLC) ID: 25058132
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Aeroheating predictions for X-34 using an inviscid-boundary layer method
By Christopher J. Riley
“Aeroheating predictions for X-34 using an inviscid-boundary layer method” Metadata:
- Title: ➤ Aeroheating predictions for X-34 using an inviscid-boundary layer method
- Author: Christopher J. Riley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics
- Publish Date: 1998
- Publish Location: ➤ Hampton, Va - [Washington, D.C - Springfield, Va - [Springfield, Va - Reston, VA
“Aeroheating predictions for X-34 using an inviscid-boundary layer method” Subjects and Themes:
- Subjects: ➤ Convective heat transfer - X-34 reusable launch vehicle - Boundary layers - Algorithms - Aerodynamic heating - Inviscid flow - Turbulent flow - Surface temperature - Mathematical models - Hypersonics
Edition Identifiers:
- The Open Library ID: OL17593122M - OL17838334M - OL17700851M - OL15539932M
- Online Computer Library Center (OCLC) ID: 40763813 - 42677791
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aeroheating predictions for X-34 using an inviscid-boundary layer method at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Hypersonic inviscid flow
By Wallace D. Hayes and Ronald F. Probstein
“Hypersonic inviscid flow” Metadata:
- Title: Hypersonic inviscid flow
- Authors: Wallace D. HayesRonald F. Probstein
- Language: English
- Number of Pages: Median: 624
- Publisher: ➤ Dover Publications, Incorporated - Dover Publications
- Publish Date: 2004 - 2012
“Hypersonic inviscid flow” Subjects and Themes:
- Subjects: ➤ Hypersonic Aerodynamics - Air flow - Mathematical models - Inviscid flow - Aerodynamics, hypersonic - Aérodynamique hypersonique - Air - Écoulement - Modèles mathématiques - Écoulement non visqueux - Überschallströmung
Edition Identifiers:
- The Open Library ID: OL38283375M - OL7639204M - OL38362664M
- Online Computer Library Center (OCLC) ID: 53021584 - 1004387561
- Library of Congress Control Number (LCCN): 2003062540
- All ISBNs: ➤ 9780486432816 - 9781306369794 - 0486160483 - 9780486160481 - 1306369797 - 0486432815
Access and General Info:
- First Year Published: 2004
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Hypersonic inviscid flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8The stability of two-dimensional wakes and shear-layers at high Mach numbers
By D. T. Papageorgiou
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Metadata:
- Title: ➤ The stability of two-dimensional wakes and shear-layers at high Mach numbers
- Author: D. T. Papageorgiou
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Shear layers - Wakes - Two dimensional flow - Hypersonic flow - Laminar flow - Flow stability - High Reynolds number - Mach number
Edition Identifiers:
- The Open Library ID: OL18263144M - OL16137874M - OL17631976M
- Online Computer Library Center (OCLC) ID: 67124982
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The stability of two-dimensional wakes and shear-layers at high Mach numbers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Supersonic diffusers - Computational grids - Two dimensional flow - Turbulence models - Navier-Stokes equation - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15414474M - OL17116401M - OL18081585M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems
By Xiao-Yen Wang
“Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems” Metadata:
- Title: ➤ Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems
- Author: Xiao-Yen Wang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Conservation - Advection - Nonlinearity - Space-time functions - Burger equation
Edition Identifiers:
- The Open Library ID: OL17584194M - OL18135651M - OL15550590M
- Online Computer Library Center (OCLC) ID: 42333066
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Finite difference calculation of an inviscid transonic flow over oscillating airfoils
By T. Ishiguro
“Finite difference calculation of an inviscid transonic flow over oscillating airfoils” Metadata:
- Title: ➤ Finite difference calculation of an inviscid transonic flow over oscillating airfoils
- Author: T. Ishiguro
- Number of Pages: Median: 43
- Publisher: Royal Aircraft Establishment
- Publish Date: 1982
- Publish Location: Farnborough, Hants, England
“Finite difference calculation of an inviscid transonic flow over oscillating airfoils” Subjects and Themes:
- Subjects: Finite difference theory - Inviscid flow - Transonic flow
Edition Identifiers:
- The Open Library ID: OL20268312M - OL21041935M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Finite difference calculation of an inviscid transonic flow over oscillating airfoils at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Multigrid calculation of three-dimensional turbomachinery flows
By D. A. Caughey
“Multigrid calculation of three-dimensional turbomachinery flows” Metadata:
- Title: ➤ Multigrid calculation of three-dimensional turbomachinery flows
- Author: D. A. Caughey
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University
- Publish Date: 1989
- Publish Location: ➤ Ithaca, New York - [Washington, D.C.] - [Springfield, Va
“Multigrid calculation of three-dimensional turbomachinery flows” Subjects and Themes:
- Subjects: ➤ Alternating direction implicit methods - Computational fluid dynamics - Computational grids - Euler equations of motion - Inviscid flow - Navier-Stokes equation - Rotor blades (Turbomachinery) - Three dimensionsal flow - Transonic flow - Turbomachine blades - Two dimensional flow
Edition Identifiers:
- The Open Library ID: OL17683518M - OL14972268M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Multigrid calculation of three-dimensional turbomachinery flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Stable boundary conditions for Cartesian grid calculations
By Martin J. Berger
“Stable boundary conditions for Cartesian grid calculations” Metadata:
- Title: ➤ Stable boundary conditions for Cartesian grid calculations
- Author: Martin J. Berger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Stable boundary conditions for Cartesian grid calculations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Grid generation (Mathematics) - Computational grids - Boundary conditions - Euler equations of motion - Cartesian coordinates
Edition Identifiers:
- The Open Library ID: OL17631974M - OL16138276M
- Online Computer Library Center (OCLC) ID: 67836530
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Stable boundary conditions for Cartesian grid calculations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
By Domenic D'Ambrosio
“A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” Metadata:
- Title: ➤ A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
- Author: Domenic D'Ambrosio
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, VA - [Springfield, Va
“A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Corner flow - Essentially non-oscillatory schemes - Flux difference splitting - Inviscid flow - Navier-Stokes equation - Supersonic flow - Three dimensional flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17791703M - OL15413863M
- Online Computer Library Center (OCLC) ID: 34061925
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A numerical method for solving the three-dimensional parabolized Navier-Stokes equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Aerodynamics of engine-airframe interaction
By David A. Coughey
“Aerodynamics of engine-airframe interaction” Metadata:
- Title: ➤ Aerodynamics of engine-airframe interaction
- Author: David A. Coughey
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Aerodynamics of engine-airframe interaction” Subjects and Themes:
- Subjects: Aerodynamic forces - Inviscid flow - Euler equations of motions - Computational grids - Transonic flow
Edition Identifiers:
- The Open Library ID: OL18078468M - OL15408082M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aerodynamics of engine-airframe interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16On computations of the integrated space shuttle flowfield using overset grids
By I.-T Chiu
“On computations of the integrated space shuttle flowfield using overset grids” Metadata:
- Title: ➤ On computations of the integrated space shuttle flowfield using overset grids
- Author: I.-T Chiu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center - Iowa State University, Engineering Research Institute
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Ames, Iowa] - [Moffett Field, Calif
“On computations of the integrated space shuttle flowfield using overset grids” Subjects and Themes:
- Subjects: ➤ Computational grids - Computerized simulation - Flow distribution - Inviscid flow - Space shuttle ascent stage - Three dimensional flow
Edition Identifiers:
- The Open Library ID: OL17725445M - OL17633025M
- Online Computer Library Center (OCLC) ID: 61493607
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find On computations of the integrated space shuttle flowfield using overset grids at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Numerical simulation of supersonic and hypersonic inlet flow fields
By D. Scott McRae
“Numerical simulation of supersonic and hypersonic inlet flow fields” Metadata:
- Title: ➤ Numerical simulation of supersonic and hypersonic inlet flow fields
- Author: D. Scott McRae
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Mars Mission Research Center, North Carolina State University
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Raleigh, N.C - Springfield, Va
“Numerical simulation of supersonic and hypersonic inlet flow fields” Subjects and Themes:
- Subjects: ➤ Algorithms - Computational fluid dynamics - Computational grids - Flow distribution - Grid generation (Mathematics) - Hypersonic inlets - Inlet flow - Inviscid flow - Supersonic inlets - Three dimensional flow - Upwind schemes (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15418943M - OL17793972M
- Online Computer Library Center (OCLC) ID: 34562883
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of supersonic and hypersonic inlet flow fields at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Evaluation of 3D inverse code using rotor 67 as test case
By T. Dang
“Evaluation of 3D inverse code using rotor 67 as test case” Metadata:
- Title: ➤ Evaluation of 3D inverse code using rotor 67 as test case
- Author: T. Dang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Evaluation of 3D inverse code using rotor 67 as test case” Subjects and Themes:
- Subjects: Inviscid flow - Rotors - Computer programs - Pressure distribution - Pressure
Edition Identifiers:
- The Open Library ID: OL15543277M - OL17597306M
- Online Computer Library Center (OCLC) ID: 41363696
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Evaluation of 3D inverse code using rotor 67 as test case at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19Wing-section optimization for supersonic viscous flows
By Cem C. Item
“Wing-section optimization for supersonic viscous flows” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flows
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flows” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aicraft design - Airfoils - Applications programs (Computers) - Computational fluid dynamics - Inviscid flow - Navier-Stokes equation - Optimization - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL18084626M - OL17078549M
- Online Computer Library Center (OCLC) ID: 34609263
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Wing-section optimization for supersonic viscous flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20Study of the velocity gradient tensor in turbulent flow
By Wei-Ping Cheng
“Study of the velocity gradient tensor in turbulent flow” Metadata:
- Title: ➤ Study of the velocity gradient tensor in turbulent flow
- Author: Wei-Ping Cheng
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Stanford, Calif.] - [Washington, DC - Springfield, Va
“Study of the velocity gradient tensor in turbulent flow” Subjects and Themes:
- Subjects: ➤ Anisotropy - Digital simulation - Eigenvalues - Euler-Cauchy equations - Inviscid flow - Tensors - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15505451M - OL17593543M
- Online Computer Library Center (OCLC) ID: 40176276
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Study of the velocity gradient tensor in turbulent flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Implicit method for the computation of unsteady flows on unstructured grids
By V. Venkatakrishnan
“Implicit method for the computation of unsteady flows on unstructured grids” Metadata:
- Title: ➤ Implicit method for the computation of unsteady flows on unstructured grids
- Author: V. Venkatakrishnan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, VA - [Springfield, Va
“Implicit method for the computation of unsteady flows on unstructured grids” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Finite difference theory - Finite volume method - Grid generation (Mathematics) - Inviscid flow - Unsteady flow - Unstructured grids (Mathematics) - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17796476M - OL15423132M
- Online Computer Library Center (OCLC) ID: 35218754
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Implicit method for the computation of unsteady flows on unstructured grids at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
By W. Kyle Anderson
“Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation” Metadata:
- Title: ➤ Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Author: W. Kyle Anderson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Computational fluid dynamics - Grid generation (Mathematics) - Inviscid flow - Navier-Stokes equation - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17593326M - OL15505120M
- Online Computer Library Center (OCLC) ID: 40173535
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23A mixed volume grid approach for the Euler and Navier-Stokes equations
By William John Coirier
“A mixed volume grid approach for the Euler and Navier-Stokes equations” Metadata:
- Title: ➤ A mixed volume grid approach for the Euler and Navier-Stokes equations
- Author: William John Coirier
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“A mixed volume grid approach for the Euler and Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Computational grids - Laminar flow - Grid generation (Mathematics) - Compressible flow - Euler equations of motion - Cartesian coordinates - Navier-Stoke equation
Edition Identifiers:
- The Open Library ID: OL18086929M - OL15423300M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A mixed volume grid approach for the Euler and Navier-Stokes equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24An inviscid computational study of an X-33 configuration at hypersonic speeds
By Ramadas K. Prabhu
“An inviscid computational study of an X-33 configuration at hypersonic speeds” Metadata:
- Title: ➤ An inviscid computational study of an X-33 configuration at hypersonic speeds
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“An inviscid computational study of an X-33 configuration at hypersonic speeds” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Viscous flow - X-33 reusable launch vehicle - Venturestar launch vehicle - Aerospike engines - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15559399M - OL17592144M
- Online Computer Library Center (OCLC) ID: 43252433
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find An inviscid computational study of an X-33 configuration at hypersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By Ramadas K. Prabhu
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Metadata:
- Title: ➤ An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Subjects and Themes:
- Subjects: ➤ Aeroshells - Computational fluid dynamics - Mars missions - Aerodynamics - Wind tunnel tests - Inviscid flow - Aerodynamic characteristics - Mach number
Edition Identifiers:
- The Open Library ID: OL17719832M - OL17621409M
- Online Computer Library Center (OCLC) ID: 54502386
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
By Ramadas K. Prabhu
“Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Metadata:
- Title: ➤ Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Subjects and Themes:
- Subjects: Aeroshells - Inviscid flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17607400M - OL17718835M
- Online Computer Library Center (OCLC) ID: 50120009
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Inviscid flow computations of several aeroshell configurations for a '07 Mars lander at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Metadata:
- Title: ➤ Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Hypersonic speed - Aerodynamic loads - Supersonic speed - Computational fluid dynamics
Edition Identifiers:
- The Open Library ID: OL17607401M - OL17718834M
- Online Computer Library Center (OCLC) ID: 50134015
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Summary report of the orbital X-34 wing static aeroelastic study
By Ramadas K. Prabhu
“Summary report of the orbital X-34 wing static aeroelastic study” Metadata:
- Title: ➤ Summary report of the orbital X-34 wing static aeroelastic study
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Summary report of the orbital X-34 wing static aeroelastic study” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Computational fluid dynamics - Free flow - X-34 reusable launch vehicle - Aerodynamic characteristics - Flexibility - Dynamic pressure - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL17607405M - OL16030672M
- Online Computer Library Center (OCLC) ID: 50133893
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Summary report of the orbital X-34 wing static aeroelastic study at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment
By M. J. Lyell
“Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment” Metadata:
- Title: ➤ Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment
- Author: M. J. Lyell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Mechanical and Aerospace Engineering Dept., West Virginia University
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC - Springfield, Va - Morgantown, WV
“Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment” Subjects and Themes:
- Subjects: ➤ Asymptotic properties - Floquet theorem - Flow stability - Fluid mechanics - Inviscid flow - Microgravity - Numerical integration - Stability tests
Edition Identifiers:
- The Open Library ID: OL17790324M - OL15404187M
- Online Computer Library Center (OCLC) ID: 32287895
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column
By M. J. Lyell
“Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column” Metadata:
- Title: ➤ Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column
- Author: M. J. Lyell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Mechanical & Aerospace Engineering Dept., West Virginia University - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va - Morgantown, WV
“Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Nonlinear systems - Fluid dynamics - Resonant frequencies - Liquid bridges - Oscillations
Edition Identifiers:
- The Open Library ID: OL17790329M - OL15404200M
- Online Computer Library Center (OCLC) ID: 32289249
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Wave number selection for incompressible parallel jet flows periodic in space
By Jeffrey Hilton Miles
“Wave number selection for incompressible parallel jet flows periodic in space” Metadata:
- Title: ➤ Wave number selection for incompressible parallel jet flows periodic in space
- Author: Jeffrey Hilton Miles
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Wave number selection for incompressible parallel jet flows periodic in space” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Parallel flow - Shear layers - Floquet theorem - Incompressible fluids - Flow stability
Edition Identifiers:
- The Open Library ID: OL17838515M - OL15503696M
- Online Computer Library Center (OCLC) ID: 41031129
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Wave number selection for incompressible parallel jet flows periodic in space at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows
By Osama A. Kandil
“Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows” Metadata:
- Title: ➤ Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University
- Publish Date: 1990
- Publish Location: Norfolk, Va - [Hampton, Va
“Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows” Subjects and Themes:
- Subjects: Dissipation - Euler equations of motion - Inviscid flow - Steady flow - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL16130438M - OL17633019M
- Online Computer Library Center (OCLC) ID: 62199508
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Development of a linearized unsteady Euler analysis for turbomachinery blade rows
By Joseph M. Verdon
“Development of a linearized unsteady Euler analysis for turbomachinery blade rows” Metadata:
- Title: ➤ Development of a linearized unsteady Euler analysis for turbomachinery blade rows
- Author: Joseph M. Verdon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Development of a linearized unsteady Euler analysis for turbomachinery blade rows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Differential equations - Axial flow - Unsteady aerodynamics - Rotor blades (Turbomachinery) - Inviscid flow - Euler equations of motion - Linearization - Surface properties - Three dimensional flow
Edition Identifiers:
- The Open Library ID: OL17792062M - OL15414585M
- Online Computer Library Center (OCLC) ID: 34041808
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Development of a linearized unsteady Euler analysis for turbomachinery blade rows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Travelling wave type flutter of flat panels in inviscid flow
By Aleksander Kornecki
“Travelling wave type flutter of flat panels in inviscid flow” Metadata:
- Title: ➤ Travelling wave type flutter of flat panels in inviscid flow
- Author: Aleksander Kornecki
- Language: English
- Number of Pages: Median: 259
- Publisher: ➤ Technion, Israel Institute of Technology, Dept. of Agricultural Engineering
- Publish Date: 1971
- Publish Location: [Haifa]
“Travelling wave type flutter of flat panels in inviscid flow” Subjects and Themes:
- Subjects: Fluid dynamics - Flutter (Aerodynamics) - Plates (Engineering) - Inviscid flow
Edition Identifiers:
- The Open Library ID: OL5339975M
- Library of Congress Control Number (LCCN): 72193668
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Travelling wave type flutter of flat panels in inviscid flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35On the ideal flow through axial turbomachine cascades
By J. Erik V. Nilsson
“On the ideal flow through axial turbomachine cascades” Metadata:
- Title: ➤ On the ideal flow through axial turbomachine cascades
- Author: J. Erik V. Nilsson
- Language: English
- Number of Pages: Median: 95
- Publish Date: 1962
“On the ideal flow through axial turbomachine cascades” Subjects and Themes:
- Subjects: Inviscid flow - Cascades (Fluid dynamics) - Turbomachines - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL5866505M
- Online Computer Library Center (OCLC) ID: 8104736
- Library of Congress Control Number (LCCN): 62050268
Access and General Info:
- First Year Published: 1962
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the ideal flow through axial turbomachine cascades at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Multigrid methods for aerodynamic problems in complex geometries
By D. A. Caughey
“Multigrid methods for aerodynamic problems in complex geometries” Metadata:
- Title: ➤ Multigrid methods for aerodynamic problems in complex geometries
- Author: D. A. Caughey
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Multigrid methods for aerodynamic problems in complex geometries” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Engine inlets - Euler equations of motion - Finite volume method - Inviscid flow - Multiblock grids - Multigrid methods - Navier-Stokes equation - Three dimensional flow - Transonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15419815M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Multigrid methods for aerodynamic problems in complex geometries at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings
By A. Das
“On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings” Metadata:
- Title: ➤ On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings
- Author: A. Das
- Number of Pages: Median: 20
- Publisher: Sine nomine
- Publish Date: 1986
- Publish Location: [S.l.]
“On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings” Subjects and Themes:
- Subjects: Delta wings - Inviscid flow - Vortex sheets
Edition Identifiers:
- The Open Library ID: OL19249658M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect
By Colin Walsh
“A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect” Metadata:
- Title: ➤ A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect
- Author: Colin Walsh
- Number of Pages: Median: 207
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1982
- Publish Location: [Downsview, Ont.]
“A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect” Subjects and Themes:
- Subjects: Airfoils - Ground effect (Aerodynamics) - Inviscid flow
Edition Identifiers:
- The Open Library ID: OL20982344M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A non-linear numerical solution to the 2-dimensional inviscid flow about a jet-flapped airfoil in ground effect at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations
By D. Sidilkover
“Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations” Metadata:
- Title: ➤ Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations
- Author: D. Sidilkover
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, VA
“Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations” Subjects and Themes:
- Subjects: Euler equations of motion - Inviscid flow - Multigrid methods - Multiblock grids
Edition Identifiers:
- The Open Library ID: OL17125841M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Advanced space propulsion system flowfield modeling
By S. D Smith
“Advanced space propulsion system flowfield modeling” Metadata:
- Title: ➤ Advanced space propulsion system flowfield modeling
- Author: S. D Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Advanced space propulsion system flowfield modeling” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Computerized simulation - Mathematical models - Boundary layer flow - Flow distribution - Nozzle flow - Plumes - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15544943M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Advanced space propulsion system flowfield modeling at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41A high order discontinuous Galerkin method for 2D incompressible flows
By Jianguo Liu
“A high order discontinuous Galerkin method for 2D incompressible flows” Metadata:
- Title: ➤ A high order discontinuous Galerkin method for 2D incompressible flows
- Author: Jianguo Liu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“A high order discontinuous Galerkin method for 2D incompressible flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Galerkin method - Two dimensional flow - Energy conservation - Error analysis
Edition Identifiers:
- The Open Library ID: OL17136930M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A high order discontinuous Galerkin method for 2D incompressible flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack
By Stephen H. Maslen
“Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack” Metadata:
- Title: ➤ Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack
- Author: Stephen H. Maslen
- Number of Pages: Median: 21
- Publisher: Langley Research Center
- Publish Date: 1974
- Publish Location: Hampton, Va
“Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack” Subjects and Themes:
- Subjects: Inviscid flow - Hypersonic flow - Space shuttles
Edition Identifiers:
- The Open Library ID: OL21499890M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Inviscid flow about blunted cones of large opening angle at angle of attack
By Stephen H. Maslen
“Inviscid flow about blunted cones of large opening angle at angle of attack” Metadata:
- Title: ➤ Inviscid flow about blunted cones of large opening angle at angle of attack
- Author: Stephen H. Maslen
- Number of Pages: Median: 14
- Publisher: Langley Research Center
- Publish Date: 1975
- Publish Location: Hampton, Va
“Inviscid flow about blunted cones of large opening angle at angle of attack” Subjects and Themes:
- Subjects: Inviscid flow - Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL21499884M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Inviscid flow about blunted cones of large opening angle at angle of attack at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations
By Murali Damodaran
“Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations” Metadata:
- Title: ➤ Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations
- Author: Murali Damodaran
- Number of Pages: Median: 262
- Publisher: Cornell University
- Publish Date: 1987
- Publish Location: [Ithaca, N.Y.?]
“Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations” Subjects and Themes:
- Subjects: Euler equations of motion - Inviscid flow - Unsteady flow - Transonic flow
Edition Identifiers:
- The Open Library ID: OL21333143M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies
By Stephen J. Shaw
“The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies” Metadata:
- Title: ➤ The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies
- Author: Stephen J. Shaw
- Number of Pages: Median: 51
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1990
- Publish Location: Hampton, Va
“The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies” Subjects and Themes:
- Subjects: Inviscid flow - Stability - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL21334858M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
By Nelson L. Sanger
“Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading” Metadata:
- Title: ➤ Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
- Author: Nelson L. Sanger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading” Subjects and Themes:
- Subjects: ➤ Compressors - Diffusion - Comparison - Boundary layers - Gas-turbines - Inviscid flow - Gas turbine engines - Reynolds number - Blades - Computation - Surface layers - Cascade flow - Stators - Compressor blades - Experimentation
Edition Identifiers:
- The Open Library ID: OL16151506M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47A numerical simulation of the inviscid flow through a counter-rotating propeller
By Mark L. Celestina
“A numerical simulation of the inviscid flow through a counter-rotating propeller” Metadata:
- Title: ➤ A numerical simulation of the inviscid flow through a counter-rotating propeller
- Author: Mark L. Celestina
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“A numerical simulation of the inviscid flow through a counter-rotating propeller” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Mathematical models - Turboprop engines - Flow characteristics - Airplanes - Turbine-propeller engines
Edition Identifiers:
- The Open Library ID: OL16151566M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A numerical simulation of the inviscid flow through a counter-rotating propeller at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48Application of a Runge-Kutta scheme for high-speed inviscid internal flows
By Anutosh Moitra
“Application of a Runge-Kutta scheme for high-speed inviscid internal flows” Metadata:
- Title: ➤ Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Author: Anutosh Moitra
- Number of Pages: Median: 24
- Publisher: ICASE
- Publish Date: 1986
- Publish Location: Hampton, Va
“Application of a Runge-Kutta scheme for high-speed inviscid internal flows” Subjects and Themes:
- Subjects: Euler equations of motion - Inviscid flow - Runge-Kutta method
Edition Identifiers:
- The Open Library ID: OL19986005M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Application of a Runge-Kutta scheme for high-speed inviscid internal flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
49Towards enhancing and delaying disturbances in free shear flows
By William O. Criminale
“Towards enhancing and delaying disturbances in free shear flows” Metadata:
- Title: ➤ Towards enhancing and delaying disturbances in free shear flows
- Author: William O. Criminale
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Towards enhancing and delaying disturbances in free shear flows” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Mixing layers (Fluids) - Wakes - Jet flow - Free flow - Incompressible fluids - Flow stability - Shear flow
Edition Identifiers:
- The Open Library ID: OL17682547M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Towards enhancing and delaying disturbances in free shear flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
50Numerical speed of sound and its application to schemes for all speeds
By Meng-Sing Liou
“Numerical speed of sound and its application to schemes for all speeds” Metadata:
- Title: ➤ Numerical speed of sound and its application to schemes for all speeds
- Author: Meng-Sing Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Numerical speed of sound and its application to schemes for all speeds” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Turbulent flow - High speed - Ideal gas - Low speed - Acoustic velocity - Multiphase flow
Edition Identifiers:
- The Open Library ID: OL15557207M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical speed of sound and its application to schemes for all speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.