Effect of a wind tunnel on the acoustic field from various aeroacoustic sources
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1897
Reference12 articles.
1. Transmission of Sound in Ducts with Thin Shear Layers—Convergence to the Uniform Flow Case
2. Kitaplioglu,C. and Shinoda, P; "Hover and Forward Flight Acoustic and Performanceof a Small-Scale Helicopter Rotor System," NASA TM-86787,1985.
3. FREQUENCY -24.0 -14.4 -4.8 4.8 14.4
Cited by 2 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. Review of acoustic measurement techniques in wind tunnels;21st Aerodynamic Measurement Technology and Ground Testing Conference;2000-06-19
2. Evaluation of discrete frequency sound in closed-test-section wind tunnels;Journal of Aircraft;1992-09
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