Roll-yaw control at high angle of attack by forebody tangential blowing
By: N. Pedreiro ... [et al.].
Contributors: Pedreiro, N.; Joint Institute for Aeronautics and Acoustics.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-201844
Publisher: Joint Institute for Aeronautics and Acoustics; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Stanford, Calif.?]; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Roll.; Yawing moments.; Wind tunnel models.; Wind tunnel tests.; Blowing.; Flow visualization.; Aircraft control.; Flight control.; Feedback control.
Other titles: Roll yaw control at high angle of attack by forebody tangential blowing
Notes: Shipping list no.: 98-0858-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.