Rotor Incoming Velocity Profile Measurements.
PENNSYLVANIA STATE UNIV UNIVERSITY PARK APPLIED RESEARCH LAB
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Boundary layer profiles were measured for various flow conditions at a position in front of a rotor. The rotor was located at the downstream end on an axisymmetric body. Results were obtained withwithout upstream appendages, withwithout upstream screen, and for an designoff design rotor flow coefficients. All tests were conducted in the 48-inch diameter wind tunnel at a nominal velocity of 80 fps. Author
- Fluid Mechanics