Item Details

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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

Availability

Library Location Map Availability Call Number
Alderman 3rd Floor East Reading Room N/A Available Non-Circ.