Item Details

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Multiple-Cycle Simulation of a Pulse Detonation Engine Ejector

S. Yungster, H.D. Perkins
Format
Book; Government Document; Microform
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
Language
English
Series
NASA/TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:211888
Description
10 pages : illustration.
Notes
  • Shipping list no.: 2003-0323-M.
  • "October 2002."
  • "Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002."
  • "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
  • "ICOMP-2002-05."
  • "AIAA-2002-3630."
  • Includes bibliographical references (pages 4-5).
Reproduction Notes
Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [2003]. 1 microfiche.
Series Statement
NASA/TM ; 2002-211888
NASA technical memorandum ; 2002-211888
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| "Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002."
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    a| "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
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    a| Technical memorandum.
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    a| Microfiche. b| [Washington, D.C.] : c| Supt. of Docs., U.S. G.P.O., d| [2003]. e| 1 microfiche.
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    a| "AIAA-2002-3630."
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    a| Detonable gas mixtures. 2| nasat
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    a| Ejectors. 2| nasat
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    a| Impulses. 2| nasat
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    a| Mass flow rate. 2| nasat
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    a| Pulse detonation engines. 2| nasat
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    a| Shock waves. 2| nasat
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    1
      
    a| Perkins, Hugh Douglas, e| author.
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    a| NASA Glenn Research Center. b| Institute for Computational Mechanics in Propulsion, e| issuing body.
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