| Title: | Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 |
| Author: | Chapman, Gary T. |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration :, 1961 |
| 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: | Aerodynamics, aircraft |
| Subject: | Aerodynamics, missiles and space vehicles |
| Subject: | Fluid mechanics |
| 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.