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Aerodynamic performance studies for supersonic cruise aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mascitti, V. R. |
| Copyright Year | 1976 |
| Description | Technical progress made in each of the disciplinary research areas affecting the design of supersonic cruise aircraft is discussed. The NASA Supersonic Cruise Aircraft Research program has supported an expanded research program in aerodynamics including an ever growing experimental data base, methodology development across the Mach number range, and sonic boom. Progress in the aerodynamics area could facilitate the choice of the highly swept subsonic leading edge, arrow wing, known for superior supersonic cruise efficiency. |
| File Size | 1357145 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023066 |
| Archival Resource Key | ark:/13960/t4fn5zc2v |
| Language | English |
| Publisher Date | 1976-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Arrow Wings Supersonic Aircraft Cost Effectiveness Body-wing Configurations Jet Aircraft Noise Aircraft Performance Aircraft Design Angle of Attack Aerodynamic Characteristics Prediction Analysis Techniques Aerodynamic Loads Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |