Publication Date:
2019-06-28
Description:
The trajectories of droplets in the air flowing past an NACA 651-212 airfoil at an angle of attack of 40 were determined. The collection efficiency, the area of droplet impingement, and the rate of droplet impingement were calculated from the trajectories and are presented herein.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
NACA-RM-E52B12
Format:
application/pdf