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  • 1
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    Unknown
    Application of HOST technology to the SSME HPFTP blade (1989)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The development of turbine blade analysis tools as they moved from research contracts under the NASA HOST (Hot Section Technology) program to a PC-based system for preliminary design and to use in evaluating the SSME HPFTP (Space Shuttle Main Engine High Pressure Fuel Turbo Pump) blade is discussed. The heat transfer and structural analysis of the blade, the development of a data base for constitutive modeling of the blade materials, including coatings, and the use of advanced nonlinear finite element methods are addressed.
    Keywords: STRUCTURAL MECHANICS
    Type: ASME PAPER 89-GT-130
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Unknown
    Engine Structural Analysis Software (2001)
    In:  CASI
    Details
    Publication Date: 2019-07-10
    Description: The report describes the technical effort to develop: (1) geometry recipes for nozzles, inlets, disks, frames, shafts, and ducts in finite element form, (2) component design tools for nozzles, inlets, disks, frames, shafts, and ducts which utilize the recipes and (3) an integrated design tool which combines the simulations of the nozzles, inlets, disks, frames, shafts, and ducts with the previously developed combustor, turbine blade, and turbine vane models for a total engine representation. These developments will be accomplished in cooperation and in conjunction with comparable efforts of NASA Glenn Research Center.
    Keywords: Aircraft Propulsion and Power
    Type: NASA/CR-2001-210968 , E-12822 , NAS 1.26:210968
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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