CFD Simulations of NASA B-2 Spray Chamber During Rocket Fire-Reference-Cited by-同舟云学术

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CFD Simulations of NASA B-2 Spray Chamber During Rocket Fire

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Kenzakowski Donald¹,Brinckman Kevin¹

Affiliation:

1. CRAFT Tech

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-790

Reference14 articles.

1. Schrage, R.W.,A TheoreticalStudy of Interphase Mass Transfer, Columbia Univ. Press, N.Y., 1953.

2. Turbulence Modeling Improvements for Jet Noise Prediction Using PIV Datasets

3. Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling

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1. Conceptual Design Model of High-Altitude Test Stand for Rocket Engines;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2016

2. Impinging Fuel Injector Atomization and Combustion Modeling;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

3. Analysis of Flame Deflector Spray Nozzles in Rocket Engine Test Stands;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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