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  • 1
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    Enhancing aeropropulsion research with high-speed interactive computing (1991)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a first generation Numerical Propulsion System Simulation (NPSS). The NPSS will provide a unique capability to numerically simulate advanced propulsion systems from nose to tail. Two essential ingredients to the NPSS are: (1) experimentally validated Computational Fluid Dynamics (CFD) codes; and (2) high performing computing systems (hardware and software) that will permit those codes to be used efficiently. To this end, NASA-Lewis is using high speed, interactive computing as a means for achieving Integrated CFD and Experiments (ICE). The development is described of a prototype ICE system for multistage compressor flow physics research.
    Keywords: COMPUTER SYSTEMS
    Type: International Symposium on Air Breathing Engines; Sept. 1-6, 1991; Nottingham
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    High-Speed Laser Anemometer (1982)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: New high-speed laser anemometer system rapidly and efficiently maps gas-flow velocities within rotating blade rows of turbomachinery. Small seed particles entrained in gas flow fluoresce when they pass through probe volume, which is the fringe pattern formed by intersecting laser beams. Transit time of particles is obtained by use of suitable optics, photomultiplier tube and electronic signal processor. Data are then sent to a minicomputer.
    Keywords: MECHANICS
    Type: LEW-13527 , NASA Tech Briefs (ISSN 0145-319X); 6; 1; P. 52
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Enhancing aeropropulsion research with high-speed interactive computing (1991)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a first generation Numerical Propulsion System Simulation (NPSS). The NPSS will provide a unique capability to numerically simulate advanced propulsion systems from nose to tail. Two essential ingredients to the NPSS are: (1) experimentally validated Computational Fluid Dynamics (CFD) codes; and (2) high performing computing systems (hardware and software) that will permit those codes to be used efficiently. To this end, NASA-Lewis is using high speed, interactive computing as a means for achieving Integrated CFD and Experiments (ICE). The development is described of a prototype ICE system for multistage compressor flow physics research.
    Keywords: COMPUTER SYSTEMS
    Type: NASA-TM-104374 , E-6179 , NAS 1.15:104374 , International Symposium on Air Breathing Engines; Sep 01, 1991 - Sep 06, 1991; Nottingham
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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