Laser Doppler velocimetry uncertainty analysis for rotor blade tip vortex measurements
Author:
Affiliation:
1. Maryland, Univ., College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-263
Reference41 articles.
1. Laser Velocimetry and Blade Pressure Measurements of a Blade‐Vortex Interaction
2. Experimental and numerical investigation of rotor aerodynamics in forward flight
3. Biggers,J. C., Lee, A., Orloff, K., and Lemmer, O. "Measurementsof Helicopter Rotor Tip Vortices," 33'd Forum,American HelicopterSociety,Washington,D.C., pp. l-l1, 1977.
4. Biggers,J.C., and Orloff, K. L. "Laser Velocimeter Measurements of the Helicopter Rotor-Induced Flow Field," 30th Forum,American HelicopterSociety,Washington,D. C., pp. l-10 , 1974.
5. Analysis of helicopter blade vortex structure by laser velocimetry
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