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
Published
1979 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
Edition Notes
| Statement | David B. Ercegovic, Propulsion Laboratory, AVRADCOM Research and Technology Laboratories, Lewis Research Center. |
| Series | NASA technical paper ; 1393, AVRADCOM technical report ; 78-41, NASA technical paper -- 1393., AVRADCOM technical report -- 78-41. |
| Contributions | United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., Propulsion Laboratory (U.S.) |
| The Physical Object | |
|---|---|
| Pagination | 20 p. : |
| Number of Pages | 20 |
| ID Numbers | |
| Open Library | OL17538801M |
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.
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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.
Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using jet A fuel eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA.
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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 .
