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:1976-07-20 Issue: Volume: Page:
ISSN:
Container-title:3rd Aeroacoustics Conference
language:
Short-container-title:

Author:

CROUCH R.¹,COUGHLIN C.¹,PAYNTER G.¹

Affiliation:

1. Boeing Commercial Airplane Co., Seattle, Wash.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1976-511

Reference14 articles.

1. Thornock, R. L. and Atvars, J. "Thrust and Acorrsric Performance of the NSC-119C.mAdvanced SST Type Noise Suppressor,"BoeingDocument No. D6-41990, October 1974.

2. Society of Automotive Engineers, Inc. "Sfandard Values of Atmospheric Absorption as a Function of Temperature and Humidity for Use in Evaluating Aircraft Flyover Noise," ARP 866. August 1964.

3. Society of Automotive Engineers, Inc."Definitions and Procedures for Computing the Perceived Noise Level ofAircraft Noise," ARP 865, October 1964.

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