Author : F. B. Gustafson
Publisher :
Page : 112 pages
File Size : 27,79 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 : 616 pages
File Size : 14,73 MB
Release : 1949
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 664 pages
File Size : 29,25 MB
Release : 1949
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 332 pages
File Size : 40,56 MB
Release : 1950
Category : Aerodynamics
ISBN :
Author : Vernon H. Gray
Publisher :
Page : 720 pages
File Size : 43,63 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 : 12,43 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 702 pages
File Size : 17,96 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 692 pages
File Size : 37,8 MB
Release : 1948
Category : Aeronautics
ISBN :
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 924 pages
File Size : 20,74 MB
Release : 1947
Category : Aeronautics
ISBN :
Author : Bruce T. Lundin
Publisher :
Page : 262 pages
File Size : 38,79 MB
Release : 1950
Category : Aeronautics
ISBN :
