Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53 /

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Bibliographic Details
Main Author:	Smith, John M. (John Milton), 1922-
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979.
Series:	NASA technical paper ; 1452.
Subjects:	Turbomachines > Diffusers > Testing. Gas-turbines > Combustion chambers > Testing. Diffusers > Aerodynamics. Turbomachines > Diffusers. Turbomachines. Testing. Gas-turbines. Diffusers.

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Call Number:	NAS 1.60: 1452
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