Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter
By: Aparjit J. Mahajan and Krishna Rao V. Kaza.
Contributors: Kaza, K. R. V.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 105414
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1992
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroelasticity.; Flutter (Aerodynamics)
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-1416-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1992. 1 microfiche.