An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight-Reference-Cited by-同舟云学术

An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight

Published:1982-01-11 Issue: Volume: Page:
ISSN:
Container-title:20th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HOROWITZ S.¹,SIGMAN R.¹,ZINN B.¹

Affiliation:

1. Georgia Institute of Technology, Atlanta, GA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1982-124

Reference25 articles.

1. Horowitz, S. J., R. K. Sigman, and 8.T. Zinn, "An Iterative Finite Element-Integral Technique for Predicting Sound Radiation from Turbofan Inlets:' AlAA Paper No. 81-1981, October 1981.

2. Tag, I. and E. Lumsdaine, "An Efficient Finite Element Technique for Sound Propagation in Axisymmetric Hard Wall Ducts Carrying High Subsonic Mach Number Flows;' AlAA Paper 78-1154,

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