Research Catalog

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients

Title
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.
Author
Sanders, Bobby W.
Publication
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.

Available Online

https://purl.fdlp.gov/GPO/gpo52217

Details

Additional Authors
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, issuing body.
  • Lewis Research Center, author.
Description
1 online resource (iii, 98 pages) : illustrations.
Series Statement
NASA technical paper ; 1531
Uniform Title
NASA technical paper ; 1531.
Subjects
Note
  • Title from title screen (viewed Sept. 22, 2014).
  • "January 1980."
  • "Performing organization, Lewis Research Center"--Technical report documentation page.
Bibliography (note)
  • Includes bibliographical references (pages 27-28).
Funding (note)
  • Sponsored by National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.60:1531
OCLC
marcive761221787
Author
Sanders, Bobby W., author.
Title
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.
Publisher
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA technical paper ; 1531
NASA technical paper ; 1531.
Bibliography
Includes bibliographical references (pages 27-28).
Funding
Sponsored by National Aeronautics and Space Administration 505-04
E-9467
Connect to:
https://purl.fdlp.gov/GPO/gpo52217
Added Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, issuing body.
Lewis Research Center, author.
Other Form:
Print version: Sanders, Bobby W. 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 (OCoLC)7959956
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:1531
View in Legacy Catalog