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Rotating turbine disk cavity flow field distribution within the system of experimental and computational studies
Author: YangXiaoLi
Tutor: FengQing
School: Northwestern Polytechnical University
Course: Thermal Power Engineering
Keywords: Rotating disk cavity Anti- pre-swirl nozzle Flow structure Intake inertial force Rotational effects
CLC: V231
Type: Master's thesis
Year: 2005
Downloads: 206
Quote: 4
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Abstract
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CLC: > Aviation, aerospace > Aviation > Aero-engine ( propulsion system ) > Engine theory
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