Computation and validation of fluid/structure twin tail buffet response
By: [Osama A. Kandil and Essam F. Sheta, C.H. Liu].
Contributors: Sheta, Essam F.; Liu, C. H. 1941-; United States. National Astronautics and Space Administration.; AIAA Applied Aerodynamics Conference (14th : 1996 : New Orleans, LA)
Series: [NASA contractor report] -- NASA-CR-203259.; NASA contractor report -- NASA CR-203259.
Publisher: National Aeronautics and Space Administration
Published: 1997
Place of publication: [Washington, D.C
Language: eng
Format: Microform
Number of pages: 10
Subjects: Buffeting (Aerodynamics); Airplanes -- Wings.; Airplanes -- Tail surfaces.; Aeroelasticity.
Other titles: Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow.
Notes: "The 14th AIAA Applied Aerodynamics Conference, New Orleans, LA-June 18-20, 1996"--P. [1].

Shipping list no.: 98-0356-M.

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

Includes bibliographical references (p. 5).

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