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Aerodynamics Supersonic
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Airplanes

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Online Results (173)
1.
Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55⁰ cropped delta wing
Author
Erickson, Gary E.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3253
Format
Books / Microforms
2.
Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
Author
Wood, Richard M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3105
Format
Books / Microforms
4.
Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
Author
Covell, Peter F.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
5.
The natural flow wing-design concept
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
6.
The natural flow wing-design concept
Author
Wood, Richard M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3193
Format
Books / Microforms
7.
Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design
Author
Carlson, Harry W.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3202
Format
Books / Microforms
8.
Viscous computations of cold air/air flow around scramjet nozzle afterbody
Author
Baysal, Oktay
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
9.
Viscous flow simulations of internal store carriage and separation final report for the period ended May 15, 1991
Author
Baysal, Oktay
Published
Norfolk, Va. : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:185343
Format
Books / Microforms
10.
The aerodynamic design of the oblique flying wing supersonic transport
Author
Van der Velden, Alexander J. M.
Published
Palo Alto, Calif. : Stanford University ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:177552
Format
Books / Microforms
11.
Fuselage design for a specified Mach-sliced area distribution
Author
Barger, Raymond L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
12.
Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment
Author
McMillin, S. Naomi (Susan Naomi)
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
13.
Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings a correlation with experiment
Author
McMillin, S. Naomi (Susan Naomi)
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3035
Format
Books / Microforms
14.
Supersonic combustion engine testbed heat lightning
Published
Houston, Tex. : Universities Space Research Association ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187010
Format
Books / Microforms
15.
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
Author
Darden, Christine M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
16.
Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration
Author
Hahne, David E. (David Edgar)
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
17.
Concept development of a Mach 3.0 high-speed civil transport
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
18.
Supersonic aerodynamics of delta wings
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
Location
Library Shelving Facility (LSF) >> NAS 1.60:2771
Format
Books
19.
Supersonic aerodynamics of delta wings
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
20.
Supersonic aerodynamics of delta wings
Author
Wood, Richard M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:2771
Format
Books / Microforms
21.
Planform effects on the supersonic aerodynamics of multibody configurations
Author
McMillin, S. Naomi (Susan Naomi)
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
22.
Study of lee-side flows over conically cambered delta wings at supersonic speeds
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
2660:pt.1
2660:pt.2
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
23.
Effect of leading-edge load constraints on the design and performance of supersonic wings
Author
Darden, Christine M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
24.
Effect of leading-edge load constraints on the design and performance of supersonic wings
Author
Darden, Christine M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:2446
Format
Books / Microforms
25.
Lee-side flow over delta wings at supersonic speeds
Author
Miller, David S.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online