The trajectories of water droplets in the air flowing past an NACA 6511004 airfoil at a n angle of attack of 0 deg were determined. The amount of water in droplet form impinging on the airfoil , the area of droplet impingement, and the rate of droplet impingement per unit area on the airfoil surface were calculated from the trajectories and presented t o cover a large range of flight and atmospheric conditions. These impingement characteristics are compared briefly with those previously reported for the same airfoil at angles of attack of 4 deg and 8 deg.
Impingement of Water Droplets on NACA 65A004 Airfoil at 0 Deg Angle of Attack
1955-11-01
Miscellaneous
No indication
English
Impingement of water droplets on NACA 65a004 airfoil at 0° angle of attack
Engineering Index Backfile | 1955
|Impingement of water droplets on NACA 65a004 airfoil at 8° angle of attack
Engineering Index Backfile | 1954
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