| Title: | A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft / |
| Author: | Silverstein, Calvin C. |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | Washington, D.C. : National Aeronautics and Space Administration, 1971 |
| Link: | page images at HathiTrust |
| No stable link: | This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links. |
| Subject: | Heat pipes |
| Subject: | Cooling |
| Subject: | Heat |
| Subject: | Leading edges (Aerodynamics) |
| Subject: | Hypersonic planes |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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