Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
By: Robert M. Bennett and Charlotte E. Walker.
Contributors: Walker, Charlotte E.; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-209104; NASA technical memorandum -- 209104..
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.; Delta wings.; Airfoil profiles.; Control surfaces.; Pitch (Inclination); Wind tunnel tests.
Notes: Shipping list no.: 99-0729-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.