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Low sonic boom design and performance of a mach 2.4/1.8 overland high speed civil transport
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Morgenstern, John M. |
| Copyright Year | 1992 |
| Description | This paper describes the design features of a Douglas Mach 2.4/1.8 Low Sonic Boom High Speed Civil Transport (HSCT) configuration developed for NASA. The configuration is designed to fly over water at Mach 2.4 for highest productivity and economic worth, and fly over land at Mach 1.8 with reduced sonic boom loudness. |
| File Size | 504306 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920076745 |
| Archival Resource Key | ark:/13960/t3130sn2z |
| Language | English |
| Publisher Date | 1992-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Productivity Loudness Shock Waves Civil Aviation Noise Reduction Aircraft Noise Supersonic Flight Economic Factors Sonic Booms Supersonic Transports Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
