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High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Koch, L. C. Pagel, L. L. |
| Copyright Year | 1978 |
| Description | The results of a program to design and fabricate an unshielded actively cooled structural panel for a hypersonic aircraft are presented. The design is an all-aluminum honeycomb sandwich with embedded cooling passages soldered to the inside of the outer moldline skin. The overall finding is that an actively cooled structure appears feasible for application on a hypersonic aircraft, but the fabrication process is complex and some material and manufacturing technology developments are required. Results from the program are summarized and supporting details are presented. |
| File Size | 5889112 |
| Page Count | 173 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790012226 |
| Archival Resource Key | ark:/13960/t7cs0mp9t |
| Language | English |
| Publisher Date | 1978-12-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Fabrication Structural Design Cooling Aluminum Fatigue Materials Honeycomb Structures Sandwich Structures Hypersonic Aircraft Aircraft Structures Heat Flux 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 |
