Experimental Pressure Distributions Over Wing Tips At Mach Number 19
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Author | : Harold Mirels |
Publisher | : |
Total Pages | : 28 |
Release | : 1949 |
Genre | : Aerodynamic load |
ISBN | : |
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.
Author | : Henry C. Lessing |
Publisher | : |
Total Pages | : 98 |
Release | : 1960 |
Genre | : Aerodynamics, aircraft |
ISBN | : |
Author | : Lowell E. Hasel |
Publisher | : |
Total Pages | : 120 |
Release | : 1959 |
Genre | : Aerodynamic load |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1064 |
Release | : 1973 |
Genre | : Aeronautics |
ISBN | : |
Author | : Alberta Y. Alksne |
Publisher | : |
Total Pages | : 56 |
Release | : 1961 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1080 |
Release | : 1966-11 |
Genre | : Government publications |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 606 |
Release | : 1986 |
Genre | : Astronautics |
ISBN | : |