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Tuesday, July 28, 2020 | History

3 edition of A sectored-one-dimensional model for simulating combustion instabilities in premix combustors found in the catalog.

A sectored-one-dimensional model for simulating combustion instabilities in premix combustors

Daniel E. Paxson

A sectored-one-dimensional model for simulating combustion instabilities in premix combustors

by Daniel E. Paxson

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  • 15 Currently reading

Published by National Aeronautics and Space Administration, Glenn Research Center, Available from NASA Center for Aerospace Information, National Technical Information Service [distributor in Cleveland, Ohio, Hanover, MD, Springfield, VA .
Written in English

    Subjects:
  • Computational fluid dynamics.,
  • Equations of motion.,
  • Combustion chambers.,
  • Combustion stability.,
  • Thermal instability.,
  • Premixed flames.

  • Edition Notes

    Other titlesSectored one dimensional model for simulating combustion instabilities in premix combustors
    StatementDaniel E. Paxson.
    SeriesNASA/TM -- 1999-209771, NASA technical memorandum -- 209771..
    ContributionsNASA Glenn Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18295725M


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A sectored-one-dimensional model for simulating combustion instabilities in premix combustors by Daniel E. Paxson Download PDF EPUB FB2

Sectored-one-dimensional model for simulating combustion instabilities in premix combustors (OCoLC) Online version: Paxson, Daniel E. Sectored-one-dimensional model for simulating combustion instabilities in premix combustors (OCoLC) Material Type: Government publication, National government publication: Document Type: Book.

Sectored-one-dimensional model for simulating combustion instabilities in premix combustors (OCoLC) Microfiche version: Paxson, Daniel E. Sectored-one-dimensional model for simulating combustion instabilities in premix combustors (OCoLC) Material Type: Document, Government publication, National government publication, Internet.

Investigation of Choking and Combustion Products' Swirling Frequency Effects on Gas Turbine Compressor Blade Fractures A Sectored One-Dimensional Model for Simulating Combustion Instabilities in Premix Combustors,” 38th Aerospace Sciences Author: E.

Poursaeidi, M. Arablu, M. Yahya Meymandi, M. Mohammadi Arhani. Lean-burning combustors are susceptible to combustion instabilities. Additionally, due to non-uniformities in the fuel-air mixing and in the combustion process, there typically exist hot areas in.

Lean combustion concepts for aircraft engine combustors are prone to combustion instabilities. Mitigation of instabilities is an enabling technology for these low-emissions combustors. Close Drawer Menu Close Drawer Menu Menu. Home; Journals. AIAA Journal; Journal of Aerospace Information Systems; Journal of Air Transportation; Journal of Aircraft; Journal of .