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Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition. part 1, Computational fluid dynamics (CFD) investigation / Shu-Cheng S. Chen.

Chen, Shu-Cheng S., (author.). NASA Glenn Research Center, (issuing body.).
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Record details

  • Physical Description: 1 online resource (iii, 37 pages).
  • Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.

Content descriptions

General Note:
"July 2017."
Bibliography, etc. Note:
Includes bibliographical references (page 37).
Formatted Contents Note:
pt. 1. Computational fluid dynamics (CFD) investigation.
Type of Report and Period Covered Note:
Technical memorandum.
Source of Description Note:
Description based on online resource; title from PDF title page (NASA, viewed Aug. 11, 2017).

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