Item Details

Experimental Investigation of Advanced Concepts to Increase Turbine Blade Loading: VII. Performance Evaluation of Modified Jet-Flap Rotor Blade

by H.G. Lueders
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Language
English
Variant Title
Performance evaluation of modified jet-flap rotor blade.
Series
NASA Contractor Report
Description
v, 27 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared by Allison Division, General Motors, for Lewis Research Center.
  • N71-20182.
  • Includes bibliographical references (p. 10).
Series Statement
NASA contractor report ; NASA CR-1759
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Experimental investigation of advanced concepts to increase turbine blade loading : b| VII. Performance evaluation of modified jet-flap rotor blade / c| by H.G. Lueders.
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    a| Performance evaluation of modified jet-flap rotor blade.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1971.
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    a| v, 27 p. : b| ill. ; c| 27 cm.
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    a| NASA contractor report ; v| NASA CR-1759
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    a| Prepared by Allison Division, General Motors, for Lewis Research Center.
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    a| Includes bibliographical references (p. 10).
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    a| Mode of access: Internet.
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    a| Turbines x| Blades x| Testing.
    650
      
    0
    a| Jet flaps (Airplanes) x| Testing.
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    a| United States. b| National Aeronautics and Space Administration.
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    a| General Motors Corporation.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106856732 y| 1971 r| pd q| bib

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