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The Turbulent Flow in Diffusers of Small Divergence AngleThe turbulent flow in a conical diffuser represents the type of turbulent boundary layer with positive longitudinal pressure gradient. In contrast to the boundary layer problem, however, it is not necessary that the pressure distribution along the limits of the boundary layer(along the axis of the diffuser) be given, since this distribution can be obtained from the computation. This circumstance, together with the greater simplicity of the problem as a whole, provides a useful basis for the study of the extension of the results of semiempirical theories to the case of motion with a positive pressure gradient. In the first part of the paper,formulas are derived for the computation of the velocity and.pressure distributions in the turbulent flow along, and at right angles to, the axis of a diffuser of small cone angle. The problem is solved.
Document ID
20050019433
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Gourzhienko, G. A.
(Tsentralni Aerogidrodinamicheskii Inst. Moscow, USSR)
Date Acquired
August 22, 2013
Publication Date
October 1, 1947
Publication Information
Publication: Central Aero-Hydrodynaical Institute Reports
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-TM-1137
Report Number: NACA-TM-1137
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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