Author : Robert A. Jones
Publisher :
Page : 44 pages
File Size : 44,8 MB
Release : 1969
Category :
ISBN :
Author : UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
Publisher :
Page : 39 pages
File Size : 26,36 MB
Release : 1965
Category :
ISBN :
Author : Robert A. Jones
Publisher :
Page : 86 pages
File Size : 30,77 MB
Release : 1969
Category :
ISBN :
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
Page : 966 pages
File Size : 47,66 MB
Release : 1970
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 962 pages
File Size : 43,81 MB
Release : 1970
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 956 pages
File Size : 22,51 MB
Release : 1970
Category : Science
ISBN :
Author :
Publisher :
Page : 402 pages
File Size : 22,67 MB
Release : 1972
Category :
ISBN :
Author :
Publisher :
Page : 1502 pages
File Size : 41,5 MB
Release : 1969
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : Lawrence E. Putnam
Publisher :
Page : 28 pages
File Size : 48,38 MB
Release : 1967
Category : Aerodynamics
ISBN :
Author : J. Wayne Keyes
Publisher :
Page : 146 pages
File Size : 35,2 MB
Release : 1973
Category : Aerodynamic heating
ISBN :
An analytical and experimental study is presented of the aerodynamic heating resulting from six types of shock interference patterns encountered in high speed flow. Centerline measurements of pressure and heat transfer distributions on basic bodies were obtained in four wind tunnels for Mach numbers from 6 to 20, specific heat ratios from 1.27 to 1.67, and free stream Reynolds numbers from 3 million to 25.6 million per meter. Peak heating and peak pressures up to 17 and 7.5 times stagnation values, respectively, were measured. In general, results obtained from semiempirical methods developed for each of the six types of interference agreed with the experimental peaks.
