Optimum Operating Parameters and Blade Setting of a High-Speed Propeller
Author:
Affiliation:
1. Polytechnic Military School, Bordj El Bahri 16046, Algeria
2. University of Sciences and Technology Houari Boumediene, Bab Ezzouar 16111, Algeria
3. University of Padova, Padova 35131, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035861
Reference41 articles.
1. GroenwegJ. F.BoderL. J. “NASA Advanced Propeller Research,” NASA TM 88969, Sept. 1988.
2. MitchellG. A. “Experimental Aerodynamic Performance of Advanced 40° swept, 10 Blade Propeller Model at Mach 0.6 to 0.85,” NASA TM 101361, 1988.
3. HagerR. D.VrabelD. “Advanced Turboprop Project,” NASA SP-495, 1988.
4. Compressible lifting surface theory for propeller performance calculation
5. Computational Fluid Dynamics Analysis of an Optimized Load-Distribution Propeller
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