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Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system by Banks, Daniel W.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [National Technical Information Service, distributor], 1987Call Number: Loading…
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2
Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser by Banks, Daniel W.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988Call Number: Loading…
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3
Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration by Banks, Daniel W.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Call Number: Loading…
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4
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system by Banks, Daniel W.
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; National Technical Information Service, distributor], 1987Call Number: Loading…
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5
Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser by Banks, Daniel W.
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1988Call Number: Loading…
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6
The F/A-18 high-angle-of-attack ground-to-flight correlation : lessons learned
[Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1997Other Authors: “…Banks, Daniel W.…”
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7
Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model by Fisher, David F.
Edwards, Calif. : [Springfield, Va. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; For sale by the National Technical Information Service], 1988Other Authors:Call Number: Loading…
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8
Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration by Paulson, John W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984Other Authors:Call Number: Loading…
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9
Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model by Fisher, David F.
Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], 1988Other Authors:Call Number: Loading…
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Related Subjects
Airplanes
Aerodynamic characteristics
Fluid dynamics
Jet planes
Testing
Thrust reversers
Aerodynamics
Aircraft performance
Angle of attack
Canard configurations
Fighter aircraft
Fighter planes
Flaps (Airplanes)
Flight control
Flight tests
Flow distribution
Low speed
Nozzles
Spanwise blowing
Trailing edge flaps
Wind tunnel tests