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Title Effects of rotation on coolant passage heat transfer [electronic resource].

Imprint [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; East Hartford, Conn. : Pratt & Whitney ; [Springfield, Va. : National Technical Information Service, distributor], 1991-1993.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4396/V.1    ---  Available
Description 2 v.
Series NASA contractor report ; 4396
NASA contractor report ; NASA CR-4396.
Note "Prepared for Lewis Research Center under contract NAS3-23691."
Form Mode of access via the NTRS web site.
Contents v. 1. Coolant passages with smooth walls / T.J. Hajek ... [et al.] -- v. 2. Coolant passages with trips normal and skewed to the flow / B.V. Johnson, J.H. Wagner, and G.D. Steuber.
Subject Heat -- Transmission.
Turbomachines -- Blades -- Cooling.
Computational fluid dynamics.
Coolants.
Cooling systems.
Heat transfer.
Mathematical models.
Pressure reduction.
Rotation.
Turbine blades.
Walls.
Added Author Hajek, T. J.
Johnson, B. V.
Wagner, J. H.
Steuber, G. D.
Lewis Research Center.
Pratt & Whitney Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:4396

 
    
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