Title: | Pressure distributions and aerodynamic characteristics of several spoiler controls on a 40 degree sweptback wing at a Mach number of 1.61 |
Author: | Landrum, Emma Jean |
Author: | Czarnecki, K. R. |
Author: | Langley Research Center |
Note: | National Aeronautics and Space Administration, 1960 |
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 characteristics |
Subject: | Aerofoils |
Subject: | Angle of attack |
Subject: | Aspect ratio |
Subject: | Pitching moments |
Subject: | Pressure distribution |
Subject: | Reynolds number |
Subject: | Spoilers |
Subject: | Supersonic speed |
Subject: | Sweptback wings |
Subject: | Tapering |
Subject: | Trailing edges |
Subject: | Wind tunnel tests |
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.