Item Details

Throat Stability-Bypass Systems to Increase the Stable Airflow Range of a Mach 2.5 Inlet With 60-Percent Internal Contraction

by Glenn A. Mitchell, Bobby W. Sanders, and Robert J. Shaw
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Language
English
Series
NASA Technical Memorandum
Description
41 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Includes bibliographical references (p. 18).
Series Statement
NASA technical memorandum ; NASA TM X-2976
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Throat stability-bypass systems to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction / c| by Glenn A. Mitchell, Bobby W. Sanders, and Robert J. Shaw.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1974.
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    a| 41 p. : b| ill. ; c| 27 cm.
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    a| NASA technical memorandum ; v| NASA TM X-2976
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    a| Prepared at Lewis Research Center.
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    a| Includes bibliographical references (p. 18).
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    a| Mode of access: Internet.
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    a| Aerodynamics, Supersonic.
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    a| Airplanes x| Turbojet engines x| Air intakes.
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    a| Shaw, Robert J. q| (Robert Joseph), d| 1946-
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106724450 y| 1974 r| pd q| bib

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