Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack
Author:
Affiliation:
1. Sverdrup Technology, Inc., Brook Park, Ohio 44142
2. NASA Lewis Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45939
Reference11 articles.
1. 2Bushnell, P., Gnuber, M., and Parzych, D. "Measurement of Unsteady Blade Surface Pressures on a Single Rotation Large Scale Advanced Propfan with Angular and Wake Inflow at Mach Numbers from 0.02to 0.70," NASA CR-182123, Oct.1988.
2. PTA flight test overview
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Prediction of Noise Field of a Propfan at Angle of Attack;Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers;1993
2. Unsteady Euler analysis of the flowfield of a propfan at an angle ofattack;Journal of Propulsion and Power;1992-01
3. Unsteady blade-surface pressures on a large-scale advanced propeller- Prediction and data;Journal of Propulsion and Power;1991-11
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