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Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lee, Christopher A. |
| Copyright Year | 1995 |
| Description | From December 1991 to June 1992, applied aerodynamic research support was given to the team working on Low Sonic Boom configurations in the RAC branch at NASA Ames Research Center. This team developed two different configurations: a conventional wing-tail and a canard wing, in an effort to reduce the overpressure of shock waves and the accompanying noise which are projected to the ground from supersonic civil transport aircraft. A generic description of this sensitive technology is given. |
| File Size | 416023 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950020231 |
| Archival Resource Key | ark:/13960/t6838qx4q |
| Language | English |
| Publisher Date | 1995-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Shock Waves Performance Tests Aerodynamic Configurations Overpressure Canard Configurations Noise Intensity Pressure Distribution Sonic Booms Supersonic Transports Design Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
