An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Engine Performance Evaluation and Risk Mitigation Study --Reference-Cited by-同舟云学术

An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Engine Performance Evaluation and Risk Mitigation Study -

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Tani Naoki,Yamanishi Nobuhiro,Kurosu Akihide,Negishi Hideyo,Daimon Yu

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. 1Kurosu, A. "Progress on the LE-X Cryogenic Booster Engine." Proceedings of the 4th European Conference for Aerospace Sciences, SaintPetersburg, Russia, July,2011.

2. 2Kawatsu, K. "Multi Objective Optimization of a Supersonic Axial Turbine Blade Row Shape for Rocket Engine Turbopump." Proceedings of 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Diego, CA, August, 2011.

3. 3Ahuja, V. "Computational Analysis of Pressurization in Cryogenic Tanks." Proceedings of 44th AIAA/ASME/SAE/ASEEJointPropulsion Conference &Exhibit, AIAA-2008-4752, Hartford,CT,July,2008.

4. 5Negishi, N., Daimon, Y., and Yamanishi, N. "Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in Subscale Thrust Chamber." Proceedings of 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit, San-Diego, CA, August, 2011.

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1. An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Influence of Coolant Leakage on Engine Power Balance -;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

2. An End-to-End HighFidelity Numerical Simulation of the LE-X Engine - Combustion Chamber Risk Evaluation -;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

3. Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in a Methane-Cooled Thrust Chamber;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30