Author : Dean R. Chapman
Publisher :
Page : 852 pages
File Size : 42,72 MB
Release : 1952
Category : Aerodynamics, Supersonic
ISBN :
The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.
Author : Dean R. Chapman
Publisher :
Page : 62 pages
File Size : 24,30 MB
Release : 1952
Category : Aerodynamics, Supersonic
ISBN :
The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1304 pages
File Size : 16,49 MB
Release : 1956
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 686 pages
File Size : 27,14 MB
Release : 1973
Category :
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 48 pages
File Size : 50,82 MB
Release : 1958
Category : Aeronautics
ISBN :
Author : United States. Wright Air Development Division
Publisher :
Page : 1440 pages
File Size : 46,21 MB
Release : 1959
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1200 pages
File Size : 18,73 MB
Release : 1954
Category : Aeronautics
ISBN :
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1208 pages
File Size : 14,24 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 534 pages
File Size : 46,6 MB
Release : 1953
Category : Aeronautics
ISBN :
Author : Frankie Gale Moore
Publisher :
Page : 218 pages
File Size : 31,75 MB
Release : 1973
Category : Guided missiles
ISBN :
Several theoretical and empirical procedures are combined into a single computer program to predict lift, drag, and center of pressure on quite general wing-body geometries. The method is applicable for Mach number zero to three and angle-of-attack zero to about fifteen degrees. Computed results for several configurations compare well with experimental and other analytical results. It costs about five dollars per Mach number to compute the static aerodynamics of a typical wing-body shape on the CDC 6700 computer.
