Title: | Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction |
Author: | Pfenninger, W. |
Author: | Syberg, J. |
Author: | Langley Research Center |
Author: | Boeing Commercial Airplane Company |
Note: | National Aeronautics and Space Administration ;, 1974 |
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: | Boundary layer |
Subject: | Jet nozzles -- Noise |
Subject: | Laminar flow |
Subject: | Supersonic wind tunnels |
Other copies: | Look for editions of this book at your library, or elsewhere. |
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