Experimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20° / / by Robert L. Stallings and Dorothy H. Tudor |
Autore | Stallings Robert L. |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 |
Descrizione fisica | 1 online resource (76 pages) : illustrations |
Collana | NASA technical note |
Soggetto topico |
Aerodynamics
Mach number Pressure distribution |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910714090003321 |
Stallings Robert L.
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Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 | ||
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Lo trovi qui: Univ. Federico II | ||
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Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / / Robert L. Stallings, Jr., and Milton Lamb |
Autore | Stallings Robert L. |
Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
Descrizione fisica | 1 online resource (45 pages) : illustrations |
Collana | NASA technical paper |
Soggetto topico |
Boundary layer flow
Boundary layer stability Heat transfer Reynolds number Wind tunnel tests Aerothermodynamics Boundary layer Supersonic wind tunnels |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910707438603321 |
Stallings Robert L.
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[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
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Lo trovi qui: Univ. Federico II | ||
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