Author : F. B. Gustafson
Publisher :
Page : 112 pages
File Size : 38,64 MB
Release : 1945
Category : Aerodynamic load
ISBN :
1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 400 pages
File Size : 50,27 MB
Release :
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 386 pages
File Size : 19,70 MB
Release : 1943
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 712 pages
File Size : 32,26 MB
Release :
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 664 pages
File Size : 33,26 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 616 pages
File Size : 19,30 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 32 pages
File Size : 45,63 MB
Release : 1946
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 332 pages
File Size : 36,79 MB
Release : 1950
Category : Aerodynamics
ISBN :
Author : Vernon H. Gray
Publisher :
Page : 720 pages
File Size : 48,47 MB
Release : 1953
Category : Aerofoils
ISBN :
The effects of primary and runback icing and frost formations on the drag of an 8-foot-chord NACA 651-212 airfoil section were investigated over a range of angles of attack from 2 degrees to 8 degrees and airspeeds up to 260 miles per hour for icing conditions with liquid-water contents ranging from 0.25 to 1.4 grams per cubic meter and datum air temperatures of -30 to 30 degrees F.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 50 pages
File Size : 32,54 MB
Release : 1949
Category : Aeronautics
ISBN :
