Influence of Nozzle Cavity on Indirect Vortex- and Entropy-Sound Production-Reference-Cited by-同舟云学术

Influence of Nozzle Cavity on Indirect Vortex- and Entropy-Sound Production

Published:2019-07 Issue:7 Volume:57 Page:3100-3103
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hirschberg L.¹,Hulshoff S. J.²,Collinet J.³,Schram C.¹,Schuller T.⁴

Affiliation:

1. von Kármán Institute for Fluid Dynamics, 1640 Sint-Genesius-Rode, Belgium

2. Delft University of Technology, 2629 HS Delft, The Netherlands

3. ArianeGroup, 78130 Les Mureaux, France

4. Institute of Fluid Mechanics of Toulouse, 31400 Toulouse, France

Funder

Association Nationale de la Recherche et de la Technologie

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J058138

Reference14 articles.

1. HirschbergL. “Low Order Modeling of Vortex Driven Self-Sustained Pressure Pulsations in Solid Rocket Motors,” Ph.D. Thesis, CentraleSupélec, Univ. Paris Saclay, France, 2019.

2. Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces

3. AnthoineJ. “Experimental and Numerical Study of Aeroacoustic Phenomena in Large Solid Propellant Boosters, with Application to the Ariane 5 Solid Rocket Motor,” Ph.D. Thesis, Free Univ. of Brussels, Brussels, 2000.

4. Instabilities and pressure oscillations in solid rocket motors

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