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Data and results from a study of internal convective cooling systems for hypersonic aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Anthony, F. M. Helenbrook, R. G. Dukes, W. H. |
| Copyright Year | 1974 |
| Description | An extensive survey of current and future airframe construction materials and coolants was conducted, so that the most promising candidates could be examined for cooled-panel, cooling-system and airframe concepts. Consideration was given to over 100 structural materials, 50 coolants, 6 classes of structural panel concepts, 4 classes of thermal panel concepts with numerous variations, and 3 overall cooled airframe design approaches, including unshielded, shielded, and dual temperature types. The concept identification and parametric comparison phase examined all major elements of the convectively cooled airframe, including the differing requirements at various locations on the aircraft. The parametric results were used for the investigation to two separate vehicles, a hypersonic transport with a length of 96 meters (314 feet) and a weight of 24,000 kg (528,600 lb) and a hypersonic research airplane, with a length of 25m (80 ft) and a weight of 20,300 kg (447,000 lb). |
| File Size | 15181990 |
| Page Count | 369 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740022309 |
| Archival Resource Key | ark:/13960/t3809vs3m |
| Language | English |
| Publisher Date | 1974-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aerodynamic Configurations Airframes Materials Tests Aerodynamic Heating Cooling Systems Aircraft Design Thermodynamic Properties Heat Sinks Hypersonic Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
