Author : Don W. Jillie
Publisher :
Page : 36 pages
File Size : 21,77 MB
Release : 1961
Category : Fluid mechanics
ISBN :
Author :
Publisher :
Page : 260 pages
File Size : 35,73 MB
Release : 1970
Category :
ISBN :
Author :
Publisher :
Page : 450 pages
File Size : 22,79 MB
Release : 1960
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 448 pages
File Size : 15,71 MB
Release : 1960
Category :
ISBN :
Author : John B. Peterson
Publisher :
Page : 28 pages
File Size : 33,15 MB
Release : 1966
Category : Skin friction (Aerodynamics)
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 43,6 MB
Release : 1960-07
Category :
ISBN :
Author : Kaufman Louis G. (II)
Publisher :
Page : 60 pages
File Size : 49,47 MB
Release : 1975
Category : Aerodynamics, Hypersonic
ISBN :
Shock-induced flow-separation ahead of trailing edge controls on swept wings is investigated with emphasis on the effects of boundary layer transition on the location and shape of the separation line. Experimental results were obtained by using forward facing steps mounted on swept-leading-edge flat-plate wing models in the ARL Mach 6 Tunnel for model running length Reynolds numbers varying from 0.9 to 33 million. The data support qualitatively a proposed, strip-type method for estimating, the extent and shape of the three dimensional region of separated flow ahead of controls on swept wings. (Author).
Author :
Publisher :
Page : 356 pages
File Size : 14,84 MB
Release : 1970
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1274 pages
File Size : 49,45 MB
Release : 1961
Category : Government publications
ISBN :
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 1540 pages
File Size : 43,94 MB
Release : 1961-10
Category : Military art and science
ISBN :
