New scaling laws for hot and cold jet mixing noise based on a geometric acoustics model

Author:

MORFEY C.1,SZEWCZYK V.1,TESTER B.2

Affiliation:

1. Southampton, University, Southampton,England

2. Lockheed-Georgia Co., Marietta, Ga.

Publisher

American Institute of Aeronautics and Astronautics

Reference84 articles.

1. Strouhai number: position of peak in axial jets: Code: A , mrwrement 5of Laufer et e l f1974): emiricdi 1.3 Cam,oarison of Lighthill afd GA S c i i o Law,

2. For given mean velocity and mean tempereture profites, equation (2.1) can be solved numerically after taking its Fourier transform with respect to t i h i l t and the axial and azimuthal coordlnates. Numerical solutions for the far-field pressure can be obtained for arbitrary values of the frequency parameter 166 -2n6/Ao, radiation angle. Bo, (or emisrlon angle, 0,) and azimuthal node number, n, radlated by stationary ring sources of arbitrary

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1. Acoustic Simulation of Hot Jets Issuing from a Rectangular Hypersonic Nozzle;Journal of Propulsion and Power;2014-05

2. Prediction of Supersonic Jet Noise Radiated from Rectangular and Axi-Symmetric Plug Nozzles;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009

3. Effects of Nozzle Scale, Total Temperature and an Afterburner on Jet Noise from a Pre-Cooled Turbojet Engine;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009

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