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ANALYSIS OF GEOMETRY AND DESIGN POINT PERFORMENCE OF AXIAL FLOW TURBINES [NASA CR-1181] : I - deveopment of the analysis method and the loss coefficient correlation

By: Contributor(s): Material type: TextTextLanguage: English Series: National Aeronutics and Space Administration (NASA)Publication details: NASA, WASHINGTON, D.C.Description: vii,107pSubject(s): DDC classification:
  • NASA CR-1181
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