Explore: Delta Wings
Discover books, insights, and more — all in one place.
Learn more about Delta Wings with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “delta-wings”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Study of lee-side flows over conically cambered delta wings at supersonic speeds
By Richard M. Wood
“Study of lee-side flows over conically cambered delta wings at supersonic speeds” Metadata:
- Title: ➤ Study of lee-side flows over conically cambered delta wings at supersonic speeds
- Author: Richard M. Wood
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office - Langley Research Center
- Publish Date: 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Study of lee-side flows over conically cambered delta wings at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Supersonic - Delta wing airplanes - Delta wings - Supersonic Aerodynamics - Supersonics
Edition Identifiers:
- The Open Library ID: OL15274155M - OL18028620M - OL19044550M
Access and General Info:
- First Year Published: 1987
- 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 lee-side flows over conically cambered delta wings at supersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Transonic Navier-Stokes calculations about a 65⁰ delta wing
By W. Kelly Londenberg
“Transonic Navier-Stokes calculations about a 65⁰ delta wing” Metadata:
- Title: ➤ Transonic Navier-Stokes calculations about a 65⁰ delta wing
- Author: W. Kelly Londenberg
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Transonic Navier-Stokes calculations about a 65⁰ delta wing” Subjects and Themes:
- Subjects: ➤ Delta wings - Leading edges - Vortices - Reynolds number - Transonic flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15409447M - OL18079111M - OL17790639M
- Online Computer Library Center (OCLC) ID: 32771918
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 Transonic Navier-Stokes calculations about a 65⁰ delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Delta wings with shock-free cross flow
By S. S. Sritharan
“Delta wings with shock-free cross flow” Metadata:
- Title: ➤ Delta wings with shock-free cross flow
- Author: S. S. Sritharan
- Language: English
- Publisher: ➤ institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“Delta wings with shock-free cross flow” Subjects and Themes:
- Subjects: ➤ Airplanes - Camber - Cross flow - Cross-flow (Aerodynamics) - Delta wings - Potential flow - Shock waves - Supersonic airfoils - Triangular Wings
Edition Identifiers:
- The Open Library ID: OL18293404M - OL16154912M
Access and General Info:
- First Year Published: 1984
- 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 Delta wings with shock-free cross flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
By Osama A. Kandil
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Metadata:
- Title: ➤ Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Norfolk, Va - Springfield, Va - [Washington, DC
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Buffeting - Computational fluid dynamics - Delta wings - Flutter - Vortices - Wing tips
Edition Identifiers:
- The Open Library ID: OL17593616M - OL15508543M
- Online Computer Library Center (OCLC) ID: 40618623
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 Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5An exact theory of supersonic flow around a delta wing
By L. R. Fowell
“An exact theory of supersonic flow around a delta wing” Metadata:
- Title: ➤ An exact theory of supersonic flow around a delta wing
- Author: L. R. Fowell
- Number of Pages: Median: 92
- Publisher: ➤ [Institute of Aerophysics] - Institute of Aerophysics
- Publish Date: 1955
- Publish Location: [Downsview, Ont.]
“An exact theory of supersonic flow around a delta wing” Subjects and Themes:
- Subjects: Conical flow - Supersonic flow - Delta wings
Edition Identifiers:
- The Open Library ID: OL20897560M - OL20985528M
Access and General Info:
- First Year Published: 1955
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find An exact theory of supersonic flow around a delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Detailed flow-field measurements over a 75⁰ swept delta wing
By Scott O. Kjelgaard
“Detailed flow-field measurements over a 75⁰ swept delta wing” Metadata:
- Title: ➤ Detailed flow-field measurements over a 75⁰ swept delta wing
- Author: Scott O. Kjelgaard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Detailed flow-field measurements over a 75⁰ swept delta wing” Subjects and Themes:
- Subjects: ➤ Vortices - Delta wings - Swept wing - Flow visualization - Jet flow - Free flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405497M - OL18077244M
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 Detailed flow-field measurements over a 75⁰ swept delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
By Long P. Yip
“Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform” Metadata:
- Title: ➤ Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
- Author: Long P. Yip
- Number of Pages: Median: 32
- Publisher: Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform” Subjects and Themes:
- Subjects: Delta wings - Remotely piloted Vehicles
Edition Identifiers:
- The Open Library ID: OL21333263M - OL21333179M
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 Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
By J. Moreira
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Metadata:
- Title: ➤ Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
- Author: J. Moreira
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Mechanical Engineering Dept., Worcester Polytechnic Institute
- Publish Date: 1995
- Publish Location: ➤ Worcester, MA - [Washington, DC - Springfield, Va
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Subjects and Themes:
- Subjects: Angle of attack - Delta wings - Spanwise blowing - Vortex breakdown - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL15419012M - OL17793986M
- Online Computer Library Center (OCLC) ID: 34612627
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 Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
By Gregory V. Selby
“Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel” Metadata:
- Title: ➤ Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel” Subjects and Themes:
- Subjects: ➤ Flow visualization - Cryogenic wind tunnels - Condensation - Low temperature engineering - Vortex-motion - Vortices - Wind tunnels - Delta wing airplanes - Delta wings - Transonic wind tunnels - Wind tunnel models
Edition Identifiers:
- The Open Library ID: OL18224346M - OL16122220M
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 Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Numerical solutions of Navier-Stokes equations for a Butler wing
By Jamshid S. Abolhassani
“Numerical solutions of Navier-Stokes equations for a Butler wing” Metadata:
- Title: ➤ Numerical solutions of Navier-Stokes equations for a Butler wing
- Author: Jamshid S. Abolhassani
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Aeronautics and Space Administration, Langley Research Center - Old Dominion University Research Foundation - National Technical Information Service, distributor
- Publish Date: 1985 - 1987
- Publish Location: ➤ Springfield, Va - [Washington, DC - Norfolk, Va - Hampton, Va
“Numerical solutions of Navier-Stokes equations for a Butler wing” Subjects and Themes:
- Subjects: ➤ Airplanes - Compressible flow - Delta wings - Flow distribution - Heat transmission - Ideal gas - Integral equations - Navier-Stokes equation - Navier-Stokes equations - Numerical analysis - Spherical coordinates - Three dimensional flow - Triangular Wings - Uniform flow - Unsteady flow - Viscous flow - Wings, Triangular
Edition Identifiers:
- The Open Library ID: OL15400560M - OL16157234M
Access and General Info:
- First Year Published: 1985
- 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 solutions of Navier-Stokes equations for a Butler wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11The art of sharp-leading-edged delta wings with blowing
By D. A. Tavella
“The art of sharp-leading-edged delta wings with blowing” Metadata:
- Title: ➤ The art of sharp-leading-edged delta wings with blowing
- Author: D. A. Tavella
- Language: English
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics - National Technical Information Service, distributor - Stanford University, Dept. of Aeronautics and Astronautics
- Publish Date: 1985
- Publish Location: ➤ Stanford, CA - [Springfield, Va
“The art of sharp-leading-edged delta wings with blowing” Subjects and Themes:
- Subjects: Delta wings - Blowing - Lift augmentation - Sharp leading edges - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL18082541M - OL15415980M
Access and General Info:
- First Year Published: 1985
- 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 art of sharp-leading-edged delta wings with blowing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
By Ken Craig
“Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Metadata:
- Title: ➤ Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Author: Ken Craig
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ Stanford University, Dept. of Aeronautics and Astronautics - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1991
- Publish Location: ➤ [Moffett Field, Calif.?] - Stanford, Calif
“Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Subjects and Themes:
- Subjects: ➤ Unsteady flow (Aerodynamics) - Airplanes - Delta wing airplanes - Control surfaces - Equilibrium flow - Upper surface blowing - Turbulence models - Wing profiles - Flow distribution - Delta wings - Grid generation (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17633070M - OL16137796M
- Online Computer Library Center (OCLC) ID: 34364710
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 Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
By Gregory Wayne Burgreen
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Metadata:
- Title: ➤ Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
- Author: Gregory Wayne Burgreen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic nozzles - Sensitivity - Delta wings - Discrete functions - Airfoils - Aerodynamic configurations - Aircraft design - Supercritical wings - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15419545M - OL18084662M
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 Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Lee-side flow over delta wings at supersonic speeds
By David S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: David S. Miller
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Supersonic speed - Leading edges - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL18217697M - OL16114989M
Access and General Info:
- First Year Published: 1985
- 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 Lee-side flow over delta wings at supersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Theoretical and experimental investigation of vortex breakdown
By E. Krause
“Theoretical and experimental investigation of vortex breakdown” Metadata:
- Title: ➤ Theoretical and experimental investigation of vortex breakdown
- Author: E. Krause
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Theoretical and experimental investigation of vortex breakdown” Subjects and Themes:
- Subjects: ➤ Delta wings - Finite difference theory - Navier-Stokes equation - Prediction analysis techniques - Vortex breakdown - Vortices
Edition Identifiers:
- The Open Library ID: OL17684284M
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 Theoretical and experimental investigation of vortex breakdown at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
By R. W. Hess
“Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” Metadata:
- Title: ➤ Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
- Author: R. W. Hess
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service,]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” Subjects and Themes:
- Subjects: ➤ Control surfaces - Delta wings - Longitudinal control - Oscillations - Pressure measurement - Steady state - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16116604M
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 Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments
By Arabindo Das
“Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments” Metadata:
- Title: ➤ Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments
- Author: Arabindo Das
- Number of Pages: Median: 24
- Publisher: DFVLR
- Publish Date: 1986
- Publish Location: Braunschweig
“Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments” Subjects and Themes:
- Subjects: Delta wings - Euler equations of motion - Inviscid flow
Edition Identifiers:
- The Open Library ID: OL19250160M
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 Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Lee-side flow over delta wings at supersonic speeds
By D. S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: D. S. Miller
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Flow visualization - Leading edges - Supersonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL18468528M
Access and General Info:
- First Year Published: 1985
- 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 Lee-side flow over delta wings at supersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19On 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.
20Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By Ira J. Walker
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Metadata:
- Title: ➤ Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
- Author: Ira J. Walker
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Subjects and Themes:
- Subjects: ➤ Stabilizers (Fluid dynamics) - Canard configurations - Hypersonics - Aerodynamic characteristics - Delta wings - Wind tunnel tests - Research vehicles - Mach number - Hypersonic vehicles - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15403234M
Access and General Info:
- First Year Published: 1993
- 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 Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Effective control of computationally simulated wing rock in subsonic flow
By Osama A. Kandil
“Effective control of computationally simulated wing rock in subsonic flow” Metadata:
- Title: ➤ Effective control of computationally simulated wing rock in subsonic flow
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Effective control of computationally simulated wing rock in subsonic flow” Subjects and Themes:
- Subjects: ➤ Control theory - Delta wings - Flux difference splitting - Difference equations - Rigid structures - Active control - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15508549M
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 Effective control of computationally simulated wing rock in subsonic flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
By Robert M. Bennett
“Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Metadata:
- Title: ➤ Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
- Author: Robert M. Bennett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Pitch (Inclination) - Airfoil profiles - Delta wings - Control surfaces - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17133246M
Author's Alternative Names:
"Bennett, Robert M. 1945-" and "Bennett, Robert M. (Robert Merrill), 1945-"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 Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
By Richard M. Wood
“Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” Metadata:
- Title: ➤ Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
- Author: Richard M. Wood
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” Subjects and Themes:
- Subjects: Delta wings - Supersonic flow - Sweptback wings - Supersonic airfoils
Edition Identifiers:
- The Open Library ID: OL17724282M
Access and General Info:
- First Year Published: 1985
- 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 Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Numerical solutions of Navier-Stokes equations for a Butler wing
By Surendra N. Tiwari
“Numerical solutions of Navier-Stokes equations for a Butler wing” Metadata:
- Title: ➤ Numerical solutions of Navier-Stokes equations for a Butler wing
- Author: Surendra N. Tiwari
- Number of Pages: Median: 44
- Publisher: ➤ Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University
- Publish Date: 1985
- Publish Location: Norfolk, Va
“Numerical solutions of Navier-Stokes equations for a Butler wing” Subjects and Themes:
- Subjects: Delta wings - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19985986M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Numerical solutions of Navier-Stokes equations for a Butler wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25The aerodynamics of delta wings of elliptical cross-section with separated flow
By Nikos J. Mourtos
“The aerodynamics of delta wings of elliptical cross-section with separated flow” Metadata:
- Title: ➤ The aerodynamics of delta wings of elliptical cross-section with separated flow
- Author: Nikos J. Mourtos
- Number of Pages: Median: 53
- Publisher: ➤ Stanford University, Dept. of Aeronautics and Astronautics
- Publish Date: 1985
- Publish Location: Stanford, Calif
“The aerodynamics of delta wings of elliptical cross-section with separated flow” Subjects and Themes:
- Subjects: Delta wings - Separated flow
Edition Identifiers:
- The Open Library ID: OL19987115M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The aerodynamics of delta wings of elliptical cross-section with separated flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Natural rolling responses of a delta wing in transonic and subsonic flows
By Margaret A. Menzies
“Natural rolling responses of a delta wing in transonic and subsonic flows” Metadata:
- Title: ➤ Natural rolling responses of a delta wing in transonic and subsonic flows
- Author: Margaret A. Menzies
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Aeronautics
- Publish Date: 1996
- Publish Location: ➤ Reston, Va - [Washington, DC - [Springfield, Va
“Natural rolling responses of a delta wing in transonic and subsonic flows” Subjects and Themes:
- Subjects: ➤ Flow equations - Fluid dynamics - Rigid structures - Subsonic flow - Swept wings - Navier-Stokes equation - Slender wings - Delta wings - Transonic flow
Edition Identifiers:
- The Open Library ID: OL15508546M
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 Natural rolling responses of a delta wing in transonic and subsonic flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
By Margaret Anne Menzies
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Metadata:
- Title: ➤ Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
- Author: Margaret Anne Menzies
- Language: English
- Publisher: ➤ Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - Washington, D.C - [Norfolk, VA
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Subjects and Themes:
- Subjects: ➤ Flow equations - Aerodynamic coefficients - Unsteady flow - Transonic flow - Swept wings - Navier-Stokes equation - Angle of attack - Delta wings - Leading edges - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15508551M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Unsteady, transonic flow around delta wings undergoing coupled and natural modes response at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
By Roger A. Lepsch
“Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Metadata:
- Title: ➤ Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
- Author: Roger A. Lepsch
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Subjects and Themes:
- Subjects: ➤ Rolling moments - Fins - Lift drag ratio - Wind tunnel tests - Subsonic flow - Angle of attack - Delta wings - Flow visualization - Wind tunnel models - Satellite control - Directional control
Edition Identifiers:
- The Open Library ID: OL15504620M
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 Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack
By Torsten Berglind
“The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack” Metadata:
- Title: ➤ The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack
- Author: Torsten Berglind
- Number of Pages: Median: 12
- Publisher: ➤ Aeronautical Research Institute of Sweden
- Publish Date: 1988
- Publish Location: Stockholm
“The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack” Subjects and Themes:
- Subjects: Delta wings - Supersonic drag
Edition Identifiers:
- The Open Library ID: OL18930487M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
By Y. C. Vigneron
“Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges” Metadata:
- Title: ➤ Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
- Author: Y. C. Vigneron
- Number of Pages: Median: 19
- Publisher: AIAA
- Publish Date: 1978
- Publish Location: New York
“Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges” Subjects and Themes:
- Subjects: Viscous flow - Delta wings - Supersonic flow - Leading edges
Edition Identifiers:
- The Open Library ID: OL19250516M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps
By B. K. Hu
“The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps” Metadata:
- Title: ➤ The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps
- Author: B. K. Hu
- Number of Pages: Median: 23
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1989
- Publish Location: Cranfield, Bedford
“The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps” Subjects and Themes:
- Subjects: Delta wings
Edition Identifiers:
- The Open Library ID: OL19167547M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing
By B. K. Hu
“The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing” Metadata:
- Title: ➤ The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing
- Author: B. K. Hu
- Number of Pages: Median: 34
- Publisher: ➤ Cranfield Institute of Technology, College of Aeronautics
- Publish Date: 1990
- Publish Location: Cranfield, Bedford
“The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing” Subjects and Themes:
- Subjects: Delta wings
Edition Identifiers:
- The Open Library ID: OL21499481M
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 performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33A visualisation study of the vortex flow around double-delta wings
By D. H. Thompson
“A visualisation study of the vortex flow around double-delta wings” Metadata:
- Title: ➤ A visualisation study of the vortex flow around double-delta wings
- Author: D. H. Thompson
- Number of Pages: Median: 12
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1985
- Publish Location: Melbourne, Vic
“A visualisation study of the vortex flow around double-delta wings” Subjects and Themes:
- Subjects: Delta wings - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL19985966M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A visualisation study of the vortex flow around double-delta wings at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34An analysis of conical augmentor/delta wing integration
By Domingo A. Tavella
“An analysis of conical augmentor/delta wing integration” Metadata:
- Title: ➤ An analysis of conical augmentor/delta wing integration
- Author: Domingo A. Tavella
- Number of Pages: Median: 22
- Publisher: ➤ Stanford University, Department of Aeronautics and Astronautics
- Publish Date: 1987
- Publish Location: Stanford, Calif
“An analysis of conical augmentor/delta wing integration” Subjects and Themes:
- Subjects: Augmentor wing - Delta wings
Edition Identifiers:
- The Open Library ID: OL20897840M
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 An analysis of conical augmentor/delta wing integration at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35The lift of sharp-leading-edged delta wings with blowing
By Domingo A. Tavella
“The lift of sharp-leading-edged delta wings with blowing” Metadata:
- Title: ➤ The lift of sharp-leading-edged delta wings with blowing
- Author: Domingo A. Tavella
- Number of Pages: Median: 17
- Publisher: ➤ Stanford University, Dept. of Aeronautics and Astronautics
- Publish Date: 1985
- Publish Location: Stanford, Calif
“The lift of sharp-leading-edged delta wings with blowing” Subjects and Themes:
- Subjects: Delta wings - Blowing - Lift augmentation - Sharp leading edges
Edition Identifiers:
- The Open Library ID: OL20899234M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The lift of sharp-leading-edged delta wings with blowing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis
By S. N. Seshadri
“Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis” Metadata:
- Title: ➤ Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis
- Author: S. N. Seshadri
- Number of Pages: Median: 63
- Publisher: DFVLR
- Publish Date: 1989
- Publish Location: Koln
“Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis” Subjects and Themes:
- Subjects: Laser anemometers - Delta wings - Velocity
Edition Identifiers:
- The Open Library ID: OL19379684M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Experimental studies of a delta wing with leading edge flaps
By Chyang S. Lee
“Experimental studies of a delta wing with leading edge flaps” Metadata:
- Title: ➤ Experimental studies of a delta wing with leading edge flaps
- Author: Chyang S. Lee
- Number of Pages: Median: 35
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics
- Publish Date: 1987
- Publish Location: Stanford, Calif
“Experimental studies of a delta wing with leading edge flaps” Subjects and Themes:
- Subjects: Delta wings - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19246963M
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 Experimental studies of a delta wing with leading edge flaps at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
By Kenichi Rinoie
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Metadata:
- Title: ➤ Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
- Author: Kenichi Rinoie
- Number of Pages: Median: 16
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Tokyo
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Subjects and Themes:
- Subjects: Vortex flaps - Delta wings - Vortex plates
Edition Identifiers:
- The Open Library ID: OL19249019M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Application of the vortex cloud method to slender, flapped delta wings
By Sejong Oh
“Application of the vortex cloud method to slender, flapped delta wings” Metadata:
- Title: ➤ Application of the vortex cloud method to slender, flapped delta wings
- Author: Sejong Oh
- Number of Pages: Median: 84
- Publisher: ➤ [Stanford University, Dept. of Aeronautics and Acoustics?]
- Publish Date: 1987
- Publish Location: [Stanford, Calif?]
“Application of the vortex cloud method to slender, flapped delta wings” Subjects and Themes:
- Subjects: Delta wings
Edition Identifiers:
- The Open Library ID: OL20897843M
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 Application of the vortex cloud method to slender, flapped delta wings at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Theoretical studies on flapped delta wings
By Sejong Oh
“Theoretical studies on flapped delta wings” Metadata:
- Title: ➤ Theoretical studies on flapped delta wings
- Author: Sejong Oh
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: ➤ [Moffett Field, Calif.] - [Springfield, Va
“Theoretical studies on flapped delta wings” Subjects and Themes:
- Subjects: ➤ Delta wings - Boundary value problems - Vortices - Mathematical models - Leading edge flaps - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15412238M
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 Theoretical studies on flapped delta wings at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
By Julio Chu
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Metadata:
- Title: ➤ Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Author: Julio Chu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure distribution - Wind tunnel tests - Subsonic speed - Slender wings - Reynolds number - Delta wings - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL15504600M
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 Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
By Julio Chu
“Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Metadata:
- Title: ➤ Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
- Author: Julio Chu
- Number of Pages: Median: 238
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Subjects and Themes:
- Subjects: Delta wings - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL19247966M
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 Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing
By Gary E. Erickson
“Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Metadata:
- Title: ➤ Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing
- Author: Gary E. Erickson
- Number of Pages: Median: 167
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Subjects and Themes:
- Subjects: Stability - Delta wings - Strakes - Vortices
Edition Identifiers:
- The Open Library ID: OL19246997M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
By M. Leroy Spearman
“Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰” Metadata:
- Title: ➤ Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
- Author: M. Leroy Spearman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1985
- Publish Location: Hampton, Va
“Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Angle of attack - Cambered wings - Circular cones - Delta wings - Mach number - Planforms - Reentry vehicles - Space vehicles - Supersonic Aerodynamics - Supersonic airfoils - Transatmospheric vehicles
Edition Identifiers:
- The Open Library ID: OL16152816M
Access and General Info:
- First Year Published: 1985
- 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 Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45Transonic Navier-Stokes calculations about a 65 degree Delta wing
By W. Kelly Londenberg
“Transonic Navier-Stokes calculations about a 65 degree Delta wing” Metadata:
- Title: ➤ Transonic Navier-Stokes calculations about a 65 degree Delta wing
- Author: W. Kelly Londenberg
- Number of Pages: Median: 67
- Publisher: Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va
“Transonic Navier-Stokes calculations about a 65 degree Delta wing” Subjects and Themes:
- Subjects: Delta wings - Turbulence models - Navier-Stokes equation - Transonic flow - Vortices
Edition Identifiers:
- The Open Library ID: OL19755349M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Transonic Navier-Stokes calculations about a 65 degree Delta wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
By Jim A. Penland
“Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0” Metadata:
- Title: ➤ Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Author: Jim A. Penland
- Language: English
- Number of Pages: Median: 144
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1979
- Publish Location: Washington, D.C
“Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamic characteristics - Computational fluid dynamics - Delta wings - Hypersonic aircraft - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL43506463M
- Online Computer Library Center (OCLC) ID: 761863635
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
By Krishnaswami Yegna Narayan
“Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” Metadata:
- Title: ➤ Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
- Author: Krishnaswami Yegna Narayan
- Number of Pages: Median: 64
- Publisher: DFVLR
- Publish Date: 1988
- Publish Location: Koln
“Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” Subjects and Themes:
- Subjects: Delta wings - Leading edges
Edition Identifiers:
- The Open Library ID: OL18928649M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48An overview of an experimental demonstration aerotow program
By James E. Murray
“An overview of an experimental demonstration aerotow program” Metadata:
- Title: ➤ An overview of an experimental demonstration aerotow program
- Author: James E. Murray
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“An overview of an experimental demonstration aerotow program” Subjects and Themes:
- Subjects: ➤ Low aspect ratio - Tethering - Launch vehicles - Wing loading - Delta wings - Towing - Flight tests - Tetherlines
Edition Identifiers:
- The Open Library ID: OL17838341M
- Online Computer Library Center (OCLC) ID: 41020002
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 An overview of an experimental demonstration aerotow program at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.