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Heat-pipe-cooled leading edges for hypersonic vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Glass, David E. |
| Copyright Year | 2006 |
| Description | Heat pipes can be used to effectively cool wing leading edges of hypersonic vehicles. . Heat-pipe leading edge development. Design validation heat pipe testing confirmed design. Three heat pipes embedded and tested in C/C. Single J-tube heat pipe fabricated and testing initiated. HPCLE work is currently underway at several locations. |
| File Size | 2846742 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080014285 |
| Archival Resource Key | ark:/13960/t3421z02g |
| Language | English |
| Publisher Date | 2006-07-12 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Fabrication Position Location Liquid Cooling Wings Heat Pipes Embedding Leading Edges Hypersonic Vehicles Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |