The Effect Of High Wing Loading On Landing Technique And Distance With Experimental Data For The B 26 Airplane
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Author | : F. B. Gustafson |
Publisher | : |
Total Pages | : 112 |
Release | : 1945 |
Genre | : 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 | : |
Total Pages | : 400 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 386 |
Release | : 1943 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 712 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 664 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 616 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 32 |
Release | : 1946 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 332 |
Release | : 1950 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Vernon H. Gray |
Publisher | : |
Total Pages | : 720 |
Release | : 1953 |
Genre | : 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 | : |
Total Pages | : 50 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |