Velocity decay and acoustic characteristics of various nozzle geometries with forward velocity

Author:

VON GLAHN U.1,GROESBECK D.1,GOODYKOONTZ J.1

Affiliation:

1. NASA, Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. In-Flight Acoustic and Performance Characteristics of Jet-Aircraft Exhaust Noise Suppressors, TN D-874, 1961, NASA, Cleveland, Ohio. 2. Ffowcs Williams, J. E. "The Noise From Turbulence Convected at

2. Flight Effects on Mixer Nozzle Design and Noise Considerations for STOL Externally Blown Flap Systems, '' TM X-68102, 1972, NASA, Cleveland, Ohio. 4. Dorsch, R. G., and Reshotko, M. "EBF Noise Tests with Engine

3. Olsen, W. A., Dorsch, R. G., and Miles, J. H. "Noise Produced i/ by a Small-scale Externally Blown Flap, ItTND-6636, 1972, NASA,

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