Our long term objective is the development of a fast and sound methodology for simulating the dynamic aeroelastic response of an aircraft during three-dimensional high-G maneuvers in transonic and supersonic airstreams. Our focus is on AIR FORCE relevant problems exemplified by a transonic/supersonic lifting body geometry performing complex multi-G maneuvers at a free-stream Mach number M00 ranging between 0.7 and 3 (0.7 </- M(infinity) </- 3).
Numerical Simulation of Three-Dimensional High-G Dynamic Maneuvers of a Complete and Flexible Aircraft Configuration
1999
10 pages
Report
No indication
English
Optimal Coordinated Maneuvers for Three-Dimensional Aircraft Conflict Resolution
Online Contents | 2002
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