Gradient-Based Propeller Optimization with Acoustic Constraints-Reference-Cited by-同舟云学术

Gradient-Based Propeller Optimization with Acoustic Constraints

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Ingraham Daniel¹,Gray Justin S.¹,Lopes Leonard V.²

Affiliation:

1. NASA Glenn Research Center

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1219

Reference19 articles.

1. Miller, C. J., and Sullivan, J. P. “Noise constraints effecting optimal propeller designs,” Tech. Rep. NASA-TM-86967, NASA Lewis Research Center, 011985. URL https://ntrs.nasa.gov/search.jsp?R=19850011613, soc. of Automotive Engr. Gen. Aviation Aircraft Meeting and Exposition; 16-19 Apr. 1985; Wichita, KS; United States.

2. Multidisciplinary Design Optimization of a Quiet Propeller

3. Optimization of Propeller Based Propulsion System

4. Tonal and Broadband Noise Calculations for Aeroacoustic Optimization of Propeller Blades in a Pusher Configuration

5. Tonal and Broadband Noise Calculations for Aeroacoustic Optimization of a Pusher Propeller

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