Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
By: Osama A. Kandil, Essam F. Sheta, and Steven J. Massey.
Contributors: Sheta, Essam F.; Massey, Steven James.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-203258.; NASA contractor report -- NASA-CR 203258.
Publisher: National Aeronautics and Space Administration
Published: 1997
Place of publication: [Washington, D.C
Language: eng
Format: Microform
Number of pages: 15
Subjects: Buffeting (Aerodynamics); Airplanes -- Wings.; Airplanes -- Tail surfaces.; Aeroelasticity.
Other titles: Twin tail Delta wing configuration buffet due to unsteady vortex breakdown flow.
Notes: Caption title.

Shipping list no.: 98-0356-M.

Originally published: [Reston, VA] : American Institute of Aeronautics ans Astronautics, Inc., 1996.

Includes bibliographical references (p. 7).

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