Determination of transonic unsteady aerodynamic loads to predict the aeroelastic stability of fighter aircraft
1997
14 S
graph. Darst
This investigation has partly been carried out under a contract awarded by the Netherlands Agency for Aerospace Programs, contract 07801N (LCO), funded by the Dutch Ministry of Defense, and partly under a subcontract from Lockheed Martin Tactical Aircraft Systems (LMTAS), Forth Worth, Texas, USA. LMTAS was operating under U.S. Air Force Office of Scientific Research (AFOSR), contract F49620-94-C-0093, which was funded by the Wright Laboratoris
This paper has been pres. at the International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, June 17-20, 1997
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English