Numerical Investigations of Heat Transfer Enhancement in a Thrust Chamber with Hot Gas Side Wall Ribs-Reference-Cited by-同舟云学术

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Numerical Investigations of Heat Transfer Enhancement in a Thrust Chamber with Hot Gas Side Wall Ribs

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Negishi Hideyo¹,Kumakawa Akinaga¹,Moriya Shinichi¹,Yamanishi Nobuhiro¹,Sunakawa Hideo¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-830

Reference8 articles.

1. 1Kurosu,A.,etal."StudyofNextBoosterEngineLE-XinJAXA,"AIAAPaper2006-4700,July2006.

2. 2Kurosu,A.,etal."LE-X-JapaneseNextLiquidBoosterEngine,"AIAAPaper2008-4665,July2008.

3. 3Fujita,M.,etal."UpperStagePropulsionSystemforH-IIALaunchVehicle,"AIAAPaper2002-4212,July2002.

4. 5Brown, W. "Enhanced Heat Transfer Rocket Combustor Technology Component Hot-Fire Test Results, " AIAA Paper 90-2182,July1990.

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1. An analytical formula evolved from thermal-structural coupling model for life prediction and structural design of reusable thrust chambers;Applied Thermal Engineering;2024-08

2. The artificial roughness effect on the thermal performance of a submerged combustion vaporizer;Applied Thermal Engineering;2024-01

3. Numerical Evaluation of Heat Transfer Enhancement in Rocket Thrust Chambers by Wall Ribs;Numerical Heat Transfer, Part A: Applications;2014-06-04

4. Numerical Simulation of Hot-Gas Side Heat Transfer Enhancement in Thrust Chambers by Wall Ribs;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

5. Numerical Simulation of Liquid Rocket Engine Thrust Chamber Regenerative Cooling;Journal of Thermophysics and Heat Transfer;2011-01

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