Research Catalog

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system

Title
Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.
Author
DeBonis, James R.
Publication
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.

Available Online

https://purl.fdlp.gov/GPO/LPS23166

Details

Additional Authors
  • Trefny, Charles J.
  • NASA Glenn Research Center, issuing body.
Description
1 online resource (18 pages) : illustrations.
Series Statement
NASA/TM ; 2001-210567
Uniform Title
NASA technical memorandum ; 2001-210567.
Alternative Title
Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
Subject
  • Air breathing boosters
  • Hypersonic speed
  • Computational fluid dynamics
  • Wind tunnel tests
  • Propulsion
  • Pressure distribution
Note
  • "February 2001."
  • "Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
  • "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (page 5).
Type of Report (note)
  • Technical memorandum.
Funding (note)
  • Sponsored by the National Aeronautics and Space Administration
Source of Description (note)
  • Description based on online resource; title from PDF title page (NASA, viewed Nov. 13, 2017).
Call Number
GPO Internet NAS 1.15:210567
OCLC
marcive1011356298
Author
DeBonis, James R., author.
Title
Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.
Publisher
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2001-210567
NASA technical memorandum ; 2001-210567.
Bibliography
Includes bibliographical references (page 5).
Type Of Report
Technical memorandum.
Funding
Sponsored by the National Aeronautics and Space Administration WU-523-61-33-00 E-12533
Connect to:
https://purl.fdlp.gov/GPO/LPS23166
Added Author
Trefny, Charles J., author.
NASA Glenn Research Center, issuing body.
Other Form:
Print version: Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 Deg-Spike Inlet to a Rocket-Based Combined-Cyc (OCoLC)640923504
Microfiche version: DeBonis, James R. Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system (OCoLC)50765193
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:210567
View in Legacy Catalog