Experiments in aircraft roll-yaw control using forebody tangential blowing
By: Nelson Pedreiro.
Contributors: Joint Institute for Aeronautics and Acoustics.
Series: JIAA TR -- 120.; [NASA contractor report] -- NASA/CR-208349.; NASA contractor report -- NASA CR-208349.
Publisher: 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
Published: 1997
Place of publication: [Stanford, Calif.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Roll.; Yaw.; Forebodies.; Flight control.; Tangential blowing.; Vortices.; Aircraft control.; Control simulation.; Angle of attack.; Flow visualization.; Wind tunnel models.; Wind tunnel tests.; Aerodynamic characteristics.; Mathematical models.; Computerized simulation.
Other titles: Experiments in aircraft roll yaw control using forebody tangential blowing.
Notes: Shipping list no.: 99-0433.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 2 microfiches.