Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 / / by Joseph H. Kemp and F. Kevin Owen |
Autore | Kemp Joseph H. |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972 |
Descrizione fisica | 1 online resource (vii, 101 pages) : illustrations |
Collana | NASA/TN |
Soggetto topico |
Jet nozzles
Turbulent boundary layer Wall pressure Wall pressure (Aerodynamics) Aerodynamics, Hypersonic |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910716571203321 |
Kemp Joseph H. | ||
Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel / / Renaldo V. Jenkins |
Autore | Jenkins Renaldo V. |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986 |
Descrizione fisica | 1 online resource (111 pages) : illustrations |
Collana | NASA/TP |
Soggetto topico |
Airfoils
Reynolds number Transonic wind tunnels Mach number Boundary layers Aerofoils - Testing Wall pressure (Aerodynamics) Boundary layer |
Soggetto genere / forma | Statistics. |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910709712803321 |
Jenkins Renaldo V. | ||
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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