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Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / / by Mary W. Jackson and K.R. Czarnecki
Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / / by Mary W. Jackson and K.R. Czarnecki
Autore Jackson Mary W.
Pubbl/distr/stampa Washington : , : National Aeronautics and Space Administration, , April 1960
Descrizione fisica 1 online resource (16 pages) : illustrations
Collana NASA technical note
Soggetto topico Reynolds number
Turbulence
Conical bodies
Supersonic boundary layers
Surface roughness effects
Transition points
Turbulent boundary layer
Turbulent flow
Wind tunnel tests
Schlieren photography
Supersonic speed
Wind tunnel models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715362303321
Jackson Mary W.  
Washington : , : National Aeronautics and Space Administration, , April 1960
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / / Percy J. Bobbitt [and four others]
Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / / Percy J. Bobbitt [and four others]
Autore Bobbitt Percy J.
Pubbl/distr/stampa Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012
Descrizione fisica 1 online resource (58 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Supersonic flow
Wind tunnel tests
Wedges
Conical bodies
Conical flow
Cylindrical bodies
Orifices
Flight tests
Flow distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704686003321
Bobbitt Percy J.  
Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui