Multi Objective Optimization of a Supersonic Axial Turbine Blade Row Shape for Rocket Engine Turbopump-Reference-Cited by-同舟云学术

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Multi Objective Optimization of a Supersonic Axial Turbine Blade Row Shape for Rocket Engine Turbopump

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:

Kawatsu Kaname,Tani Naoki,Shimagaki Mitsuru,Uchiumi Masaharu,Yamanishi Nobuhiro,Mitsuhashi Katsunori,Mizuno Tsutomu

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. 1Kurosu, A., et al. "LE-X -Japanese Next Liquid Booster Engine-", 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA2008-4665, July2008.

2. 2G. P. Sutton, "Turbopumps, a Historical Perspective,", 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,AIAA2006-5033, July2006.

3. The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines

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