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

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
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.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.60:1452
NAS 1.60:1452	Available Place a Hold