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Sunday, July 26, 2020 | History

2 edition of Toward improved durability in advanced aircraft engine hot sections found in the catalog.

Toward improved durability in advanced aircraft engine hot sections

Toward improved durability in advanced aircraft engine hot sections

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  • 18 Currently reading

Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Aircraft gas-turbines.,
  • Aerodynamic heating.

  • Edition Notes

    StatementD.E. Sokolowski, editor.
    SeriesNASA technical memorandum -- 4087.
    ContributionsSokolowski, D. E., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15280846M

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Toward improved durability in advanced aircraft engine hot sections Download PDF EPUB FB2

Toward Improved Durability in Advanced Aircraft Engine Hot Sections Paperback – January 1, by D. Sololowski (Author) See all formats and editions Hide other formats and editions. Price New from Used from Paperback Author: D. Sololowski. Get this from a library. Toward improved durability in advanced aircraft engine hot sections.

[D E Sokolowski; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.;]. Get this from a library. Toward improved durability in advanced aircraft engine hot sections: presented at the ASME Turbo Expo--Land, Sea & Air, the 33rd ASME International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, the Netherlands, June[D E Sokolowski; ASME International Gas Turbine Institute.

Aircraft Committee.;]. Toward improved durability in advanced aircraft engine hot sections [microform] / D.E. Sokolowski, editor; Reynolds number effects on pressure loss and turbulence characteristics of four tube-bundle heat exchang Development and testing of airfoils for high-altitude aircraft [microform]: final report /.

The General Electric F is an American afterburning turbofan engine in pound (98 kN) thrust class produced by GE F originated from GE's widely used F turbofan, enlarged and improved for use in the Boeing F/AE/F Super engine was developed from the F non-afterburning turbofan planned for the A Avenger II, before it was run: The book recommends the immediate expansion of research on advanced aircraft that travel at subsonic speeds and research on designs that will meet expected future demands for supersonic and short-haul aircraft, including helicopters, commuter aircraft, "tiltrotor," and other advanced vehicle designs.

PMCs are of interest for colder sections of the engine, while CMCs are of interest for the engine hot section and the exhaust nozzle. While PMCs have been used for noncritical components (eg, ducts and piping) for a long time, there has been a steady growth in the application of PMCs for critical turbine engine components since or so, with Cited by: 3.

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The Stirling engine (or Stirling's air engine as it was known at the time) was invented and patented in It followed earlier attempts at making an air engine but was probably the first put to practical use when, inan engine built by Stirling was employed pumping water in a quarry.

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Silicon-based ceramics are attractive materials for use in gas turbine engine hot sections due to their high temperature mechanical and physical properties as well as lower density than metals.

The advantages of utilizing ceramic hot section components include weight reduction, and improved efficiency as well as enhanced power output and lower. Vehicle Efficiencies—Engine, Weight, Electrification With the increasing demands on improved fuel economy, safety and CO 2 footprint, Ford Motor Company is striving to make vehicles more efficient.

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@article{osti_, title = {Development of nondestructive evaluation methods for ceramic coatings.}, author = {Ellingson, W A and Deemer, C and Sun, J G and Erdman, S and Muliere, D and Wheeler, B}, abstractNote = {Various nondestructive evaluation (NDE) technologies are being developed to study the use of ceramic coatings on components in the hot-gas path of advanced low-emission gas-fired.

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Following a similar mechanism to the corner radius (i.e., the consolidation of the plies causing a change in part thickness, and hence, the change to the geometry of the plies, resulting in the generation of excess Cited by: