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Dynamic Response of a Mach 2.5 Axisymmetric Inlet and Turbojet Engine With a Poppet-Valve-Controled Inlet-Stability Bypass System When Subjected to Internal and External Airflow Transients

Bobby W. Sanders
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1531
Description
iii, 98 p. : ill. ; 27 cm.
Notes
  • "Lewis Research Center."
  • "January 1980"--Cover.
  • Includes bibliographical references.
Series Statement
NASA technical paper 1531
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients / c| Bobby W. Sanders.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Office ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1980.
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    a| Includes bibliographical references.
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    a| Airplanes x| Turbojet engines x| Air intakes.
    650
      
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    a| Airplanes x| Motors x| Valves.
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