Explore: Interactional Aerodynamics
Discover books, insights, and more — all in one place.
Learn more about Interactional Aerodynamics with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “interactional-aerodynamics”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
By A. A. Boretti
“Three-dimensional Euler time accurate simulations of fan rotor-stator interactions” Metadata:
- Title: ➤ Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Author: A. A. Boretti
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ Lewis Research Centre - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion
- Publish Date: 1990
- Publish Location: ➤ [Cleveland, Ohio - Cleveland, Ohio - Springfield, Va
“Three-dimensional Euler time accurate simulations of fan rotor-stator interactions” Subjects and Themes:
- Subjects: ➤ Three dimensional flow - Unsteady flow (Aerodynamics) - Unsteady aerodynamics - Turbomachinery - Flow distribution - Euler equations of motion - Rotor stator interactions - Rotor dynamics - Interactional aerodynamics - Stators
Edition Identifiers:
- The Open Library ID: OL19246815M - OL17630435M - OL16124000M - OL18226226M
- Online Computer Library Center (OCLC) ID: 59760034
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 Three-dimensional Euler time accurate simulations of fan rotor-stator interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Rotor-fuselage interactions
By Barry, John D.
“Rotor-fuselage interactions” Metadata:
- Title: Rotor-fuselage interactions
- Author: Barry, John D.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Rotor-fuselage interactions” Subjects and Themes:
- Subjects: Fuselages - Rotary wing aircraft - Proving - Interactional aerodynamics - Experimentation
Edition Identifiers:
- The Open Library ID: OL15503758M - OL17579578M - OL18121092M
- Online Computer Library Center (OCLC) ID: 41172616
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 Rotor-fuselage interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer
By Thomas F. Balsa
“Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer” Metadata:
- Title: ➤ Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer
- Author: Thomas F. Balsa
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer” Subjects and Themes:
- Subjects: ➤ Base flow - Flow stability - Interactional aerodynamics - Mixing layers (Fluids) - Shear flow - Supersonic flow - Vortex sheets
Edition Identifiers:
- The Open Library ID: OL15411630M - OL17790780M
- Online Computer Library Center (OCLC) ID: 32920327
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 Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Non-linear unsteady wing theory
By J. E. McCune
“Non-linear unsteady wing theory” Metadata:
- Title: ➤ Non-linear unsteady wing theory
- Author: J. E. McCune
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Non-linear unsteady wing theory” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - Computational fluid dynamics - Unsteady flow - Control surfaces - Interactional aerodynamics - Wings - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17683867M - OL18080139M
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 Non-linear unsteady wing theory at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Rotorcraft application of advanced computational aerodynamics
By Sharon K. Stanaway
“Rotorcraft application of advanced computational aerodynamics” Metadata:
- Title: ➤ Rotorcraft application of advanced computational aerodynamics
- Author: Sharon K. Stanaway
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service - MCAT Institute
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - San Jose, Calif - [Moffett Field, Calif
“Rotorcraft application of advanced computational aerodynamics” Subjects and Themes:
- Subjects: ➤ Vortex-motion - Computational fluid dynamics - Viscous flow - Unsteady flow - Computational grids - Rotary wing aircraft - Grid generation (Mathematics) - Interactional aerodynamics
Edition Identifiers:
- The Open Library ID: OL17725525M - OL17628475M
- Online Computer Library Center (OCLC) ID: 61730699
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 Rotorcraft application of advanced computational aerodynamics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
By D. O. Davis
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Metadata:
- Title: ➤ Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Flow measurement - Mass flow - Oblique shock waves - Boundary layer control - Boundary layer transition - Interactional aerodynamics - Slots - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15541815M - OL17838705M
- Online Computer Library Center (OCLC) ID: 41323463
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 Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Acoustic and aerodynamic study of a pusher-propeller aircraft model
By Paul T. Soderman
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Metadata:
- Title: ➤ Acoustic and aerodynamic study of a pusher-propeller aircraft model
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 59
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Aeroacoustics - Aircraft models - Aircraft wakes - Interactional aerodynamics - Noise - Propeller blades - Propeller noise - Wakes (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135237M
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 Acoustic and aerodynamic study of a pusher-propeller aircraft model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Numerical calculations of shock-wave/boundary-layer flow interactions
By P. G. Huang
“Numerical calculations of shock-wave/boundary-layer flow interactions” Metadata:
- Title: ➤ Numerical calculations of shock-wave/boundary-layer flow interactions
- Author: P. G. Huang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Numerical calculations of shock-wave/boundary-layer flow interactions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Corner flow - Boundary layer flow - K-epsilon turbulence model - Interactional aerodynamics - Supersonic flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15419320M
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 Numerical calculations of shock-wave/boundary-layer flow interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
By William J. Devenport
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Metadata:
- Title: ➤ The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
- Author: William J. Devenport
- Language: English
- Publisher: ➤ Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, VA
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Subjects and Themes:
- Subjects: ➤ Helicopters - Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Statistical distributions - Noise prediction - Blade-vortex interaction - Aerodynamic noise - Turbulent wakes - Interactional aerodynamics - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL15479176M
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 The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep
By Donald B. Hanson
“Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep” Metadata:
- Title: ➤ Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep
- Author: Donald B. Hanson
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep” Subjects and Themes:
- Subjects: ➤ Noise prediction - Turbofan engines - Homogeneous turbulence - Rotors - Interactional aerodynamics - Stators - Engine noise - Cascade flow
Edition Identifiers:
- The Open Library ID: OL16025805M
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 Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Instabilities originating from suction holes used for laminar flow control (LFC)
By Jonathan H. Watmuff
“Instabilities originating from suction holes used for laminar flow control (LFC)” Metadata:
- Title: ➤ Instabilities originating from suction holes used for laminar flow control (LFC)
- Author: Jonathan H. Watmuff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Instabilities originating from suction holes used for laminar flow control (LFC)” Subjects and Themes:
- Subjects: ➤ Flow stability - Interactional aerodynamics - Laminar boundary layer - Porous boundary layer control - Suction - Tollmien-Schlichting waves - Vortices - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15407471M
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 Instabilities originating from suction holes used for laminar flow control (LFC) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12A two dimensional study of rotor/airfoil interaction in hover
By Chyang Sheng Lee
“A two dimensional study of rotor/airfoil interaction in hover” Metadata:
- Title: ➤ A two dimensional study of rotor/airfoil interaction in hover
- Author: Chyang Sheng Lee
- Language: English
- Publisher: ➤ Stanford University - National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: ➤ Moffett Field, Calif - [Palo Alto, Calif.] - [Springfield, Va
“A two dimensional study of rotor/airfoil interaction in hover” Subjects and Themes:
- Subjects: ➤ Hovering - Hovercraft ground effect machines - Airfoil profiles - Ground effect (Aerodynamics) - Two dimensional models - Interactional aerodynamics
Edition Identifiers:
- The Open Library ID: OL15409844M
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 A two dimensional study of rotor/airfoil interaction in hover at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Blade-mounted flap control for BVI noise reduction proof-of-concept test
“Blade-mounted flap control for BVI noise reduction proof-of-concept test” Metadata:
- Title: ➤ Blade-mounted flap control for BVI noise reduction proof-of-concept test
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Blade-mounted flap control for BVI noise reduction proof-of-concept test” Subjects and Themes:
- Subjects: ➤ Helicopters - Aeroacoustics - Aircraft control - Pressure distribution - Wind tunnel tests - Flaps (Control surfaces) - Blade-vortex interaction - Noise reduction - Interactional aerodynamics - Active control
Edition Identifiers:
- The Open Library ID: OL17576249M
- Online Computer Library Center (OCLC) ID: 40169456
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 Blade-mounted flap control for BVI noise reduction proof-of-concept test at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.