Acoustic shielding and interaction effects for strongly heated supersonic twin jets

Author:

Pineau P.1ORCID,Bogey C.1ORCID

Affiliation:

1. Univ Lyon, École Centrale de Lyon, INSA Lyon, Université Claude Bernard Lyon I, CNRS, Laboratoire de Mécanique des Fluides et d’Acoustique, UMR 5509, F-69134 Ecully, France

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Reference47 articles.

1. Launch vehicle acoustics. II - Statistics of the time domain data

2. A. R. Timmins and R. E. Heuser, “A study of first-day space malfunctions,” Technical Report No. NASA-TN-D-6474, G-1038, NASA, 1971.

3. Measurement of acoustic shielding by a turbulent jet

4. Analytical model of jet shielding

5. Reduction of peak jet noise using jet refraction

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1. Numerical Simulation of the Noise Radiated by Free Hot Supersonic Twin Jets;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

2. An investigation into the scaling law of converging length for compressible round twin-jet;Physics of Fluids;2022-03

3. Supersonic jet noise from launch vehicles: 50 years since NASA SP-8072;The Journal of the Acoustical Society of America;2022-02

4. Aeroacoustic Fields of Supersonic Twin Jets at the Ideally Expanded Condition;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2021

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