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Development of an apparatus for wind tunnel dynamic experiments at high-α by Pedreiro, Nelson
[Stanford, Calif.] : [Springfield, Va.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [National Technical Information Service, distributor], 1997Call Number: Loading…
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Experiments in aircraft roll-yaw control using forebody tangential blowing by Pedreiro, Nelson
[Stanford, Calif.] : [Springfield, Va.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [National Technical Information Service, distributor], 1997Call Number: Loading…
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Roll-yaw control at high angle of attack by forebody tangential blowing
[Stanford, Calif.?] : [Washington, DC] : [Springfield, Va.] : Joint Institute for Aeronautics and Acoustics ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Other Authors: “…Pedreiro, Nelson…”
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Related Subjects
Aircraft control
Wind tunnel tests
Angle of attack
Flight control
Flow visualization
Roll
Wind tunnel models
Aerodynamic characteristics
Aerodynamic loads
Blowing
Computerized simulation
Control simulation
Degrees of freedom
Feedback control
Forebodies
Mathematical models
Support systems
Tangential blowing
Vortices
Yaw
Yawing moments