| Title: | Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 degree delta wing |
| Alternate title: | Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70° delta wing |
| Author: | Driver, Cornelius |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| 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: | Airplanes -- Wings, Triangular -- Testing |
| Subject: | Mach number |
| Subject: | Stability of airplanes |
| 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.