Impact of Injector Mass Flow Fluctuations on Combustion Dynamics in Liquid Engines-Reference-Cited by-同舟云学术

Impact of Injector Mass Flow Fluctuations on Combustion Dynamics in Liquid Engines

Published:2015-09 Issue:5 Volume:52 Page:1417-1429
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Sattelmayer Thomas¹,Schmid Martin¹,Schulze Moritz¹

Affiliation:

1. Department of Thermodynamics, Technical University of Munich, 85748 Garching, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33287

Reference14 articles.

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2. SchmidM. “Thermoakustische Kopplungsmechanismen in Flüssigkeitsraketentriebwerken,” Ph.D. Thesis, Dept. of Thermodynamics, Technical Univ. of Munich, Munich, 2014.

3. HarrjeD. T.ReardonF. H. (eds.), “Liquid Propellant Rocket Combustion Instability,” NASA SP-194, 1972.

4. LefebvreA. H., Atomization and Sprays, Hemisphere, New York, 1989, pp. 87–99.

5. Design support for advanced storable propellant engines by ROCFLAM analyses

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