Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / / A. Neal Watkins [and three others] |
Autore | Watkins A. Neal |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2015 |
Descrizione fisica | 1 online resource (20 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Cryogenics
Pressure sensitive paints Temperature sensitive paints Transonic wind tunnels Laminar flow airfoils |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910704157203321 |
Watkins A. Neal
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Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2015 | ||
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Lo trovi qui: Univ. Federico II | ||
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Quantitative global heat transfer in a Mach-6 quiet tunnel / / John P. Sullivan [and ten others] |
Autore | Sullivan John P. |
Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
Descrizione fisica | 1 online resource (148 pages) : color illustrations |
Collana | [NASA contractor report] |
Soggetto topico |
Heat transfer
Hypersonic speed Temperature sensitive paints Wind tunnel tests Hypersonic wind tunnels Heat flux Mathematical models |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702091603321 |
Sullivan John P.
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Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
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Lo trovi qui: Univ. Federico II | ||
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