Computation and validation of fluid/structure twin tail buffet response [microform] / [Osama A. Kandil and Essam F. Sheta, C.H. Liu]

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Bibliographic Details
Main Author:	Kandil, Osama A.
Corporate Authors:	United States. National Astronautics and Space Administration, AIAA Applied Aerodynamics Conference
Other Authors:	Sheta, Essam F., Liu, C. H. (Chen-Huei), 1941-
Other title:	Cover title: Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow.
Format:	Government Document Conference Proceeding Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [National Aeronautics and Space Administration], [1997]
Series:	NASA contractor report ; NASA CR-203259.
Subjects:	Buffeting (Aerodynamics) Airplanes > Wings. Airplanes > Tail surfaces. Aeroelasticity.

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Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:203259
NAS 1.26:203259	Restricted Place a Hold