Loading...
Please wait, while we are loading the content...
Similar Documents
Thermal design for areas of interference heating on actively cooled hypersonic aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Herring, R. L. Stone, J. E. |
| Copyright Year | 1978 |
| Description | Numerous actively cooled panel design alternatives for application in regions on high speed aircraft that are subject to interference heating effects were studied. Candidate design concepts were evaluated using mass, producibility, reliability and inspectability/maintainability as figures of merit. Three design approaches were identified as superior within certain regimes of the matrix of design heating conditions considered. Only minor modifications to basic actively cooled panel design are required to withstand minor interference heating effects. Designs incorporating internally finned coolant tubes to augment heat transfer are recommended for moderate design heating conditions. At severe heating conditions, an insulated panel concept is required. |
| File Size | 6557744 |
| Page Count | 174 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780012174 |
| Archival Resource Key | ark:/13960/t8dg1jf49 |
| Language | English |
| Publisher Date | 1978-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Structural Design Panels Thermal Protection Temperature Effects Aerodynamic Heating Design Analysis Hypersonic Aircraft Structural 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 |
