The Online Books Page

Effects of wall cooling and angle of attack on boundary-layer transition on sharp cones at M[mathematical symbol for infinity] = 7.4

Title:Effects of wall cooling and angle of attack on boundary-layer transition on sharp cones at M[mathematical symbol for infinity] = 7.4
Author:
Author:
Author:
Note:National Aeronautics and Space Administration ;, 1972
  
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:Boundary layer
Subject:Cone -- Aerodynamics
Subject:Heat -- Transmission
Subject:Laminar flow
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.