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Author Nagamatsu, H. T.

Title Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [electronic resource] / by H.T. Nagamatsu and R. E. Duffy.

Imprint Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:174667    ---  Available
Description 1 online resource (iii, 39 p.) : digital, PDF file
Series NASA contractor report ; 174667
NASA contractor report ; NASA CR-174667.
Note "April 1984."
"Prepared for National Aeronautics and Space Administration, Lewis Research Center under grant no. NAS3-292."
Bibliography Includes bibliographical references (p. 36-39).
Subject Circular cylinders.
Gas turbines.
Heat flux.
Heat transfer.
High pressure.
Pressure gradients.
Shock tubes.
Vanes.
Added Author Duffy, R. E.
Rensselaer Polytechnic Institute.
Lewis Research Center.
Other Form: Microfiche version: Nagamatsu, H. T. Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes. 1 microfiche. (OCoLC)688604806
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:174667

 
    
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