Reduction in Thomas Force of Rocket Turbopump Turbine by Using Robust Design Process

An application of robust design process for reduction in Thomas force of rocket turbopump turbines is presented in this paper. Because of its special specification, rocket turbopump turbines are designed as supersonic impulse turbines, and as a result, these blades have higher loading. In such a hig...

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Veröffentlicht in:	Turbomachinery 2012, Vol.40(6), pp.350-358
Hauptverfasser:	TAKIDA, Junya, FUNAZAKI, Ken-ichi, UCHIUMI, Masaharu, SHIMAGAKI, Mitsuru
Format:	Artikel
Sprache:	eng ; jpn
Schlagworte:	Blades Gas Turbine Reduction Robust Design Rocket Turbopump Rockets Specifications Thomas Force Turbines Turbopumps Vibration Vibration control
Online-Zugang:	Volltext
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