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Computer-aided space shuttle orbiter wing design study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Glatt, C. R. Phillips, W. P. Decker, J. P. Rau, T. R. |
| Copyright Year | 1974 |
| Description | An analytical and experimental investigation has been made to provide a space shuttle orbiter wing design that met the guideline requirements of landing performance, stability, and hypersonic trim for a specified center-of-gravity envelope. The analytical study was facilitated by the use of the Optimal Design Integration system (ODIN) and the experimental part of the investigation was conducted in the Langley low-turbulence pressure tunnel and the Langley continuous-flow hypersonic tunnel. |
| File Size | 4475689 |
| Page Count | 92 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740014398 |
| Archival Resource Key | ark:/13960/t2q57cg3h |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Spacecraft Performance Wing Planforms Wind Tunnel Tests Hypersonic Wind Tunnels Space Shuttle Orbiters Spacecraft Design Spacecraft Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |