Title: | Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method |
Author: | Mohn, Larry Wayne |
Author: | Langley Research Center |
Author: | Boeing Commercial Airplane Company |
Note: | National Aeronautics and Space Administration ;, 1975 |
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: | Aerodynamic load |
Subject: | Aerodynamics |
Subject: | Airplanes -- Nacelles |
Subject: | Jet transports -- Design and construction |
Other copies: | Look for editions of this book at your library, or elsewhere. |
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.