Tory II-C performance as a function of flight mach number and inlet pressure recovery

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In a parameter study involving thrust vs. flight Mach number, M.D. Mintz has found that net jet thrust becomes a maximum at about Mach 3.66 if the Tory II-C design value of inlet pressure recovery is used at all Mach numbers. This is not a realistic situation, however, because the attainable pressure recovery decreases markedly with increasing Mach number. The effect of more realistic pressure recovery values are presented in this paper. Two sets of values were employed, which differ by two percent. Diffuser operation is always critical; i.e. we are using a ``rubber`` diffuser. Nozzle are has been optimized ... continued below

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9 p.

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Moyer, J. H. January 1, 1963.

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Description

In a parameter study involving thrust vs. flight Mach number, M.D. Mintz has found that net jet thrust becomes a maximum at about Mach 3.66 if the Tory II-C design value of inlet pressure recovery is used at all Mach numbers. This is not a realistic situation, however, because the attainable pressure recovery decreases markedly with increasing Mach number. The effect of more realistic pressure recovery values are presented in this paper. Two sets of values were employed, which differ by two percent. Diffuser operation is always critical; i.e. we are using a ``rubber`` diffuser. Nozzle are has been optimized for each operating condition. Reactor parameters and nozzle area-thrust dependence information is also presented.

Physical Description

9 p.

Notes

OSTI as DE97050854

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  • Other Information: PBD: Jan 1963

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  • Other: DE97050854
  • Report No.: UCRL-ID--125502
  • Grant Number: W-7405-ENG-48
  • DOI: 10.2172/435307 | External Link
  • Office of Scientific & Technical Information Report Number: 435307
  • Archival Resource Key: ark:/67531/metadc680969

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Office of Scientific & Technical Information Technical Reports

Reports, articles and other documents harvested from the Office of Scientific and Technical Information.

Office of Scientific and Technical Information (OSTI) is the Department of Energy (DOE) office that collects, preserves, and disseminates DOE-sponsored research and development (R&D) results that are the outcomes of R&D projects or other funded activities at DOE labs and facilities nationwide and grantees at universities and other institutions.

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  • January 1, 1963

Added to The UNT Digital Library

  • July 25, 2015, 2:20 a.m.

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  • Nov. 25, 2015, 5:53 p.m.

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Moyer, J. H. Tory II-C performance as a function of flight mach number and inlet pressure recovery, report, January 1, 1963; United States. (digital.library.unt.edu/ark:/67531/metadc680969/: accessed November 17, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.