Tests Of Two Blade Propellers In The Langley 8 Foot High Speed Tunnel To Determine The Effect On Propeller Performance Of A Modification Of Inboard Pitch Distribution
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| Author | : James Benjamin Delano |
| Publisher | : |
| Total Pages | : 724 |
| Release | : 1951 |
| Genre | : Propellers, Aerial |
| ISBN | : |
This paper presents propeller characteristics for two propellers that differ only in inboard pitch distribution. The forward Mach number range extended to 0.062 and the blade-angle range was from 20 to 55 degrees. Section thrust-coefficient data are also presented to afford a more detailed analysis of the effects of modifying the pitch distribution of the inboard sections of a propeller.
| Author | : James B. Delano |
| Publisher | : |
| Total Pages | : 60 |
| Release | : 1945 |
| Genre | : |
| ISBN | : |
| Author | : John Vernon Becker |
| Publisher | : |
| Total Pages | : 204 |
| Release | : 1980 |
| Genre | : Government publications |
| ISBN | : |
| Author | : John V Becker |
| Publisher | : |
| Total Pages | : 204 |
| Release | : 1980 |
| Genre | : Aerodynamics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 498 |
| Release | : 1952 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 750 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1016 |
| Release | : 1951 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 810 |
| Release | : 1952 |
| Genre | : Mechanics, Applied |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 500 |
| Release | : 1951 |
| Genre | : Science |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 162 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
