EFFECT OF COMBUSTOR INLET GEOMETRY ON ACOUSTIC SIGNATURE AND FLOW FIELD BEHAVIOUR OF THE LOW SWIRL INJECTOR [electronic resource]

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Bibliographic Details
Online Access:	Online Access
Corporate Author:	Lawrence Berkeley National Laboratory (Researcher)
Format:	Government Document Electronic eBook
Language:	English
Published:	Berkeley, Calif. : Oak Ridge, Tenn. : Lawrence Berkeley National Laboratory. Environmental Energy Technologies Division ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2009.
Subjects:	Flames. Combustion Chambers. Combustion. Instability. Geometry. Gas Turbines. Acoustics. Shear. Combustors. Stability. Vortices. Oscillations.

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Call Number:	E 1.99:lbnl-3142e
E 1.99:lbnl-3142e	Available