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Meeting the challenges with the douglas aircraft company aeroelastic design optimization program (adop)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rommel, Bruce A. |
| Copyright Year | 1989 |
| Description | 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. |
| File Size | 468187 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890015851 |
| Archival Resource Key | ark:/13960/t21c6wb8t |
| Language | English |
| Publisher Date | 1989-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Aircraft Models Computer Graphics Flaps Control Surfaces Aerodynamics Animation Shapes Aeroelasticity Computer Aided Design Optimization Hypersonic Vehicles Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
