Low Speed Experimental Investigation Of A Thin Faired Double Wedge Airfoil Section With Nose And Trailing Edge Flaps
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| Author | : Leonard M. Rose |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1949 |
| Genre | : Aerofoils |
| ISBN | : |
A faired, double-wedge airfoil section, 4.23 percent thick, was investigated with plain nose and trailing-edge flaps. The nose flap was 0.16 chord of the airfoil and the trailing-edge flap was 0.25 chord of the airfoil. Section lift, drag, and pitching-momnet data are presented for a Reynolds number of 5,800,000 which corresponded to a Mach number of 0.17.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 472 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 988 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
| Author | : |
| Publisher | : |
| Total Pages | : 620 |
| Release | : 1945 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 996 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : P. W. Kuhns |
| Publisher | : |
| Total Pages | : 736 |
| Release | : 1957 |
| Genre | : Aerodynamics |
| ISBN | : |
Equations are derived to evaluate the effects of thermal vibration relaxation and specific-heat changes on pneumatic-probe pyrometer measurements in the region 1000 to 3000 degrees K and 0.3
| Author | : |
| Publisher | : |
| Total Pages | : 1838 |
| Release | : 1949 |
| Genre | : Government publications |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 332 |
| Release | : 1950 |
| Genre | : Science |
| ISBN | : |
| Author | : John D. Stanitz |
| Publisher | : |
| Total Pages | : 712 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with straight blades. A seventh example is presented for incompressible flow. The solutions also applye to radial-flow turbines with rotation and flow direction reversed. The effects of variations in following parameters were investigated: (1) flow rate, (2) impeller-tip speed, (3) variation of passage height with radius, and (4) number of blades. The numerical results are presented in plots of the streamlines, constant Mach number lines, and constant pressure-ratio lines. Correlation equations are developed whereby the flow conditions in any impeller with straight blades can be determined for all operating conditions.
| Author | : |
| Publisher | : |
| Total Pages | : |
| Release | : 1948 |
| Genre | : Government publications |
| ISBN | : |
