Author : Charles F. Whitcomb
Publisher :
Page : 286 pages
File Size : 15,56 MB
Release : 1961
Category :
ISBN :
Author : Donald D. Arabian
Publisher :
Page : 88 pages
File Size : 19,76 MB
Release : 1960
Category : Aerodynamics, Transonic
ISBN :
The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
Author : Don D. Davis (Jr.)
Publisher :
Page : 22 pages
File Size : 29,32 MB
Release : 1955
Category : Aerodynamics, Transonic
ISBN :
Author : Bernard E. Cunningham
Publisher :
Page : 48 pages
File Size : 11,43 MB
Release : 1962
Category : Aerodynamics
ISBN :
Author : Ralph P. Bielat
Publisher :
Page : 44 pages
File Size : 45,54 MB
Release : 1951
Category : Aerodynamics, Transonic
ISBN :
Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.
Author :
Publisher :
Page : 526 pages
File Size : 19,7 MB
Release : 1975
Category :
ISBN :
Author : Alexander D. Hammond
Publisher :
Page : 26 pages
File Size : 10,12 MB
Release : 1954
Category : Airplanes
ISBN :
Author : Ivan D. Ertel
Publisher :
Page : 292 pages
File Size : 25,66 MB
Release : 1969
Category : Government publications
ISBN :
Author : Marvin P. Fink
Publisher :
Page : 44 pages
File Size : 41,43 MB
Release : 1961
Category :
ISBN :
Author : Roland D. English
Publisher :
Page : 20 pages
File Size : 18,78 MB
Release : 1954
Category : Ailerons
ISBN :
