The Online Books Page

Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies

Title:Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies
Author:
Author:
Author:
Author:
Note:National Advisory Committee for Aeronautics, 1957
  
Link:
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:Aerofoils -- Testing
Subject:Airplanes -- Fuselage
Subject:Airplanes -- Models -- Testing
Subject:Airplanes -- Wings, Swept-back
Subject:Charts, diagrams, etc.
Subject:Wind tunnel testing
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.