An overview of the Aeroelastic Design Optimization Program (ADOP) at the Douglas Aircraft Company is given. A pilot test program involving the animation of mode shapes with solid rendering as well as wire frame displays, a complete aircraft model of a high-altitude hypersonic aircraft to test ADOP procedures, a flap model, and an aero-mesh modeler for doublet lattice aerodynamics are discussed.
Meeting the Challenges with the Douglas Aircraft Company Aeroelastic Design Optimization Program (ADOP)
1989
10 pages
Report
No indication
English
Aeroelastic design optimization program
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