NASA NTRS · 19910040156
A synchronous strobed laser light sheet for helicopter model rotor flow visualization
Abstract
A synchronous, strobed laser light sheet has been developed for use in flow visualization of a helicopter rotor model. The light sheet strobe circuit included selectable blade position, strobe duration, and multiple pulses per revolution for rotors having 2 to 9 blades. The flow was seeded with propylene glycol. Between runs, a calibration grid board was placed in the plane of the laser sheet and recorded with the video camera at the position used to record the flow field. A slip-sync mode permitted slow motion visualization of the flow field over complete rotations of the rotor. The system was used to make two-dimensional flow field cuts of a four-bladed rotor operating at advance ratio of 0.37 at wind tunnel speeds up to 79.25 meters per second (260 feet per second).
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Leighty, Bradley D., Rhodes, David B., Jones, Stephen B., Franke, John M.. 1990-01-01. A synchronous strobed laser light sheet for helicopter model rotor flow visualization. https://ntrs.nasa.gov/citations/19910040156
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