Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.

"Advantages of flight at high angles of attack include increased maneuverability and lift capabilities. These are beneficial not only for fighter aircraft, but also for future supersonic and hypersonic transport aircraft during take-off and landing. At high angles of attack the aerodynamics of...

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Bibliographic Details

Main Author:	Pedreiro, Nelson
Corporate Author:	Joint Institute for Aeronautics and Acoustics
Other title:	Experiments in aircraft roll yaw control using forebody tangential blowing.
Format:	Government Document Microfilm Book
Language:	English
Published:	[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], [1997]
Series:	NASA contractor report ; NASA CR-208349. JIAA TR ; 120.
Subjects:	Wind tunnel models. Roll. Yaw. Forebodies. Flight control. Tangential blowing. Vortices. Aircraft control. Control simulation. Angle of attack. Flow visualization. Wind tunnel tests. Aerodynamic characteristics. Mathematical models. Computerized simulation.