Explore: Turboengines

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Source: The Open Library

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1Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading

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“Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading” Metadata:

  • Title: ➤  Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading
  • Author:
  • Language: English
  • Number of Pages: Median: 129
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - [Springfield, Va

“Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1979
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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2Unsteady flows in a single-stage transonic axial-flow fan stator row

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“Unsteady flows in a single-stage transonic axial-flow fan stator row” Metadata:

  • Title: ➤  Unsteady flows in a single-stage transonic axial-flow fan stator row
  • Author:
  • Language: English
  • Number of Pages: Median: 200
  • Publisher: ➤  U.S. Army Aviation Systems Command - National Aeronautics and Space Administration - For sale by the National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [St. Louis, MO] - [Washington, D.C.]

“Unsteady flows in a single-stage transonic axial-flow fan stator row” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1986
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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