Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow /

Bibliographic Details
Main Author:	Kandil, Osama A.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Sheta, Essam F., Massey, Steven James
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : [National Aeronautics and Space Administration], [1997]
Series:	NASA contractor report ; NASA-CR 203258.
Subjects:	Buffeting (Aerodynamics) Airplanes > Wings. Airplanes > Tail surfaces. Aeroelasticity.