The unsteady aerodynamics due to vortex breakdown are studied, with application to a 65-degree delta wing. At high angles of attack, the flow field response to changes in attitude contains multiple time scales. Furthermore, severe nonlinearities are present which further complicate aerodynamic modeling. The implications for wind tunnel testing and aerodynamic modeling are discussed.
Dynamics of Aerospace Vehicles -- Nonlinear Flight Mechanics
2000
54 pages
Report
No indication
English
Aerospace vehicles and adaptive flight control
Engineering Index Backfile | 1962
|Dynamical flight path optimization of aerospace vehicles
AIAA | 1986
|Detection of Hydrogen Aboard Aerospace Flight Vehicles
NTIS | 1964
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