Publikationsdatum:
2013-08-31
Beschreibung:
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.
Schlagwort(e):
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Materialart:
NASA. Langley Research Center, Recent Advances in Multidisciplinary Analysis and Optimization, Part 3; p 1369-1378
Format:
application/pdf
