並列タイトル等Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
一般注記"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
Physical description for original version: [2], 10 p.
書誌注記Includes bibliographical references (p. 5)
原資料等に関する注記原資料の出版事項: [Washington, D.C. : National Aeronautics and Space Administration, 1997]
SUPTDOC番号: NAS 1.26: 203259
テクニカルリポート番号: AIAA 96-2517-CP
GPO管理番号: 0830-H-14 (MF)