Nozzle Exit Flow Profile Shaping for Jet Noise Reduction-Reference-Cited by-同舟云学术

Nozzle Exit Flow Profile Shaping for Jet Noise Reduction

Published:1977-09 Issue:9 Volume:14 Page:860-867
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Crouch R. W.¹,Coughlin C. L.¹,Paynter G. C.²

Affiliation:

1. Boeing Commerical Airplane Company, Seattle, Wash.

2. Boeing Aerospace Company, Seattle, Wash.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.58866

Reference12 articles.

1. 3Society of Automotive Engineers, Inc. "Standard Values of Atmospheric Absorption as a Function of Temperature and Humidity for Use in Evaluating Aircraft Flyover Noise," ARP 866, Aug. 1964.

2. 5Society of Automotive Engineers, Inc. "Definitions and Procedures for Computing the Perceived Noise Level of Aircraft Noise," ARP 865, Oct. 1964.

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