Last edited by Nezshura
Saturday, July 25, 2020 | History

3 edition of Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems found in the catalog.

Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems

Jane M. Manderscheid

Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems

by Jane M. Manderscheid

  • 182 Want to read
  • 4 Currently reading

Published by National Aeronautics and Space Administration in [Washington, DC?] .
Written in English

    Subjects:
  • Turbines -- Blades.,
  • Space vehicles -- Propulsion systems.

  • Edition Notes

    StatementJane M. Manderscheid and Albert Kaufman.
    SeriesNASA technical memorandum -- 86990.
    ContributionsKaufman, Albert, 1928-, United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17658807M

      Structural Characteristics and Design Technical Keys of Wind Turbine Foundation in Shanghai Donghai-Bridge Offshore Wind Farm Deep Foundations and Geotechnical In Situ Testing April Energy Generation Efficiency and Strength Coupled Design and . Space Propulsion Analysis and Design by Humble, Ronald and a great selection of related books, art and collectibles available now at - Space Propulsion Analysis and Design by Humble, Ronald - AbeBooks.

    Thanks for contributing an answer to Space Exploration Stack Exchange! Please be sure to answer the question. Provide details and share your research! But avoid Asking for help, clarification, or responding to other answers. Making statements based on opinion; back them up with references or personal experience. Use MathJax to format equations. This paper provides an overview of the aircraft turbine engine control research at NASA Glenn Research Center (GRC). A brief introduction to the engine control problem is first provided with a description of the state-of-the-art control law structure.

    Model (CRM)b, which was designed without the propulsion system in place, is used as a starting point and optimized with the attached pylon and engine nacelle employing a gradient-based algorithm on local design parameters. For a gradient-based optimization to be e cient, the evaluation of the gradient itself has to be e Size: 2MB. The performance of the whole aircraft must also be considered with the combined interactions between the power and propulsion systems. The larger loading demands placed on the power and propulsion subsystems result in thrust, speed, and altitude transients that affect the whole aircraft. This results in different operating parameters for the.


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Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems by Jane M. Manderscheid Download PDF EPUB FB2

Anisotropic high-temperature alloys are used to meet the safety and durability requirements of turbine blades for high-pressure turbopumps in reusable space propulsion systems. Get this from a library. Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems.

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Select an Price: $ temperature. As shown in the diagram, some of the air is used to cool the turbine nozzles, by a combination of internal convection cooling and film cooling, processes that will be discussed in detail below.

Another portion of the cooling air is transferred onto the rotor and used to cool the rotating blades and their supporting disc. For the fan stream, there is no turbine, so let us repeat the argument.

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