Effects of yaw and pitch motion on model attitude measurements
By: Ping Tcheng, John S. Tripp, and Tom D. Finley.
Contributors: Tripp, John S.; FInley, Tom D.; Langley Research Center.
Series: NASA technical memorandum -- 4641.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft models.; Angular velocity.; Computational fluid dynamics.; Dimensional measurement.; Dynamic response.; Mathematical models.; Pitching moments.; Wind tunnel tests.; Yaw.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0478-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.