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Record Nr. |
UNINA9910699736203321 |
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Autore |
Nagamatsu Henry T. -2006 |
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Titolo |
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 |
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Pubbl/distr/stampa |
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Troy, N.Y. : , : Rensselaer Polytechnic Institute, , [1984] |
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Descrizione fisica |
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1 online resource (iii, 39 pages) : digital, PDF file |
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Collana |
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NASA contractor report ; ; 174667 |
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Altri autori (Persone) |
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Soggetti |
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Circular cylinders |
Gas turbines |
Heat flux |
Heat transfer |
High pressure |
Pressure gradients |
Shock tubes |
Vanes |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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"April 1984." |
"Prepared for National Aeronautics and Space Administration, Lewis Research Center under grant no. NAS3-292." |
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Nota di bibliografia |
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Includes bibliographical references (pages 36-39). |
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