Blended Fan Blade Effects on Aerodynamic Forces
Author:
Affiliation:
1. Wright State University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1182
Reference9 articles.
1. Fundamentals of Jet Propulsion with Applications
2. A method of predicting the performance deterioration of a compressorcascade due to sand erosion
3. Comparison of the Sensitivity to Foreign Particle Ingestion of the GE-F101 and P/W-F100 Engines to Modern Aircraft Engines
4. The influences of foreign object damage on the high cycle fatigue behavior of titanium alloy TC4
5. Probabilistic Study of Integrally Bladed Rotor Blends using Geometric Mistuning Models
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3. Design Space Exploration of Rotor Blades Accounting for Vibratory Responses by Indirect Emulation;Journal of Computing and Information Science in Engineering;2021-02-09
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