Author : William D. Deveikis
Publisher :
Page : 30 pages
File Size : 25,48 MB
Release : 1961
Category : Fluid mechanics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 12,69 MB
Release : 1960-07
Category :
ISBN :
Author :
Publisher :
Page : 1878 pages
File Size : 33,73 MB
Release : 1961
Category : Government publications
ISBN :
Author : Albert L. Braslow
Publisher :
Page : 624 pages
File Size : 36,92 MB
Release : 1958
Category : Airplanes
ISBN :
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
Author : Charles B. Rumsey
Publisher :
Page : pages
File Size : 45,73 MB
Release : 1961
Category :
ISBN :
Author : Benjamine J. Garland
Publisher :
Page : 36 pages
File Size : 33,25 MB
Release : 1962
Category : Aerodynamics
ISBN :
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 1540 pages
File Size : 37,37 MB
Release : 1961-10
Category : Military art and science
ISBN :
Author : N. S. Diaconis
Publisher :
Page : 31 pages
File Size : 40,93 MB
Release : 1957
Category : Boundary layer
ISBN :
Local heat-transfer parameters were measured on a hemisphere-cone-cylinder and on a 120 degree-included-angle cone-cylinder at a free-stream Mach number of 3.12 and at free-stream unit Reynolds numbers as high as 1,292.000 per inch. Heat-transfer data are presented for the case of wall temperature approximat&ly equal to free-stream static temperature.
Author : Louis S. Stivers
Publisher :
Page : 32 pages
File Size : 18,43 MB
Release : 1960
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 962 pages
File Size : 49,17 MB
Release : 1962
Category : Aeronautics
ISBN :
