Experimental results of wind tunnel tests on a rectangular wing panel and on a half delta wing submitted to oscillations are described. Charts of nonstationary wing pressures, of flow deflection at the trailing edge of the wing and visualizations of the wing wake are presented. A second series of tests carried out on a flying scale model of the Rafale aircraft are described. The wing pressures and local flow over the wing are quantified for flight close to the ground and in meteorologically perturbed conditions. The results of these tests are presented.
Aerodynamique Instationnaire du Vol en Milieu Turbulent. Rapport de Synthese Final (Nonstationary Flight Aerodynamics in a Turbulent Environment)
1990
72 pages
Report
Keine Angabe
Englisch
SLUB | 1956
|Turbulent boundary layers over nonstationary plane boundaries
TIBKAT | 1978
|