Effect of thermodynamic parameter on cavitation in rocket inducer
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Bibliographic Information
Effect of thermodynamic parameter on cavitation in rocket inducer
（宇宙航空研究開発機構研究開発資料, JAXA-RM-12-006E）
Japan Aerospace Exploration Agency, 2013
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ロケット用インデューサのキャビテーションに与える熱力学的パラメータの影響
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Note
Other title from p. [1]
Other authors: Kengo Kikuta, Kazuki Niiyama, Satoshi Watanabe
Includes bibliographical references (p. 33-35)