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Friday, May 15, 2020 | History

2 edition of Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel found in the catalog.

Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel

David B Ercegovic

Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel

by David B Ercegovic

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  • 15 Currently reading

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

    Subjects:
  • Aircraft gas-turbines,
  • Air -- Pollution

  • Edition Notes

    StatementDavid B. Ercegovic, Propulsion Laboratory, AVRADCOM Research and Technology Laboratories, Lewis Research Center
    SeriesNASA technical paper ; 1393, AVRADCOM technical report ; 78-41, AVRADCOM technical report -- 78-41
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Office, United States. Army Research and Technology Laboratories. Propulsion Laboratory
    The Physical Object
    Pagination20 p. :
    Number of Pages20
    ID Numbers
    Open LibraryOL17979171M


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Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel by David B Ercegovic Download PDF EPUB FB2

Tests were conducted using jet A fuel at an inlet pressure of megapascal, an inlet temperature of K, and an isothermal static pressure drop of 3 percent. Oxides of nitrogen were reduced by over 50 percent with a mixing venturi with no performance penalties in either other gaseous emissions or pressure : National Aeronautics and Space Administration NASA.

Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel. [Washington]: National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va.

An experimental investigation was conducted to determine the effect of a swirler- mounted mixing venturi on the emissions of a flame-tube combustor.

The primary zone equivalence ratio was varied from the lean blowout limit to near stoichiometric values. Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel (NASA technical paper) [David B Ercegovic] on *FREE* shipping on Author: David B Ercegovic.

Buy Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel (NASA technical paper) by David B Ercegovic (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : David B Ercegovic. David B Ercegovic has written: 'Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel' -- subject(s): Pollution, Aircraft gas-turbines, Air.

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Noté /5. Retrouvez Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using jet A fuel et des millions de livres en Format: Broché. Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using jet A fuel | National Aeronautics and Space Administration NASA | ISBN: | Kostenloser Versand für alle Bücher mit Versand und Verkauf duch : Taschenbuch.

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Liquid air. See also what's at Wikipedia, your library, or elsewhere. Broader terms: Air; Liquefied gases; Narrower term: Liquid oxygen; Used for: Air, Liquid; Filed. Full text of "Monthly catalog of United States government publications" See other formats.

Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using jet A fuel. NASA Technical Reports Server (NTRS) Ercegovic, D. Six headplate modules in a flame-tube combustor were evaluated. A mathematical model for jet engine combustor pollutant emissions. NASA Technical Reports Server (NTRS) Boccio, J.

L.; Weilerstein, G.; Edelman, R. The modules used in the model 2 assembly with a short mixing venturi installed on the downsteam side of each module are shown in figure4(c). The purpose of the venturi was twofold: First, to reduce the flow area of the outer swirler and thus increasethe combustor pressure loss; and second, to enhance mixing of the fuel and air in the wake of.

Achieving good atomization and fuel-air mixing is critical for efficient combustion, low emissions, and good temperature uniformity into the turbine. Normally, the fuel is injected in the front end of the combustor and flow recirculation is created to provide a .Full text of "NASA scientific and technical publications: A catalog of Special Publications, Reference Publications, Conference Publications, and .