Download Aerodynamic design of a free power turbine for a 75 KW gas turbine automotive engine - National Aeronautics and Space Administration NASA | PDF Online

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A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The design specifications are given and the aerodynamic design procedure is described. The design includes the transition duct and the turbine exit diffuser. The aerodynamic information includes typical results of a parametric study, velocity diagrams, blade surface and wall

Title : Aerodynamic design of a free power turbine for a 75 KW gas turbine automotive engine
Author : National Aeronautics and Space Administration NASA
Language : en
Rating :
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Type : PDF, ePub, Kindle
Uploaded : Apr 06, 2021

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