Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
By: Robert M. Bennett and Charlotte E. Walker.
Contributors: Walker, Charlotte E.; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-209130.; NASA technical memorandum -- 209130.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Unsteady aerodynamics.; Rectangular wings.; Supercritical wings.; Wing oscillations.; Wind tunnel tests.; Aircraft parts.
Notes: Shipping list no.: 1999-0729-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 2 microfiches.