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The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 / / by Paige B. Burbank and Robert W. Byrne
The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 / / by Paige B. Burbank and Robert W. Byrne
Autore Burbank Paige B.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953
Descrizione fisica 1 online resource (37 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Nozzles - Fluid dynamics
Mach number
Supersonic nozzles - Design and construction
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910713892903321
Burbank Paige B.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953
Materiale a stampa
Lo trovi qui: Univ. Federico II
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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer
Autore Beckwith Ivan E.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952
Descrizione fisica 1 online resource (30 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Nozzles - Fluid dynamics
Supersonic nozzles - Design and construction
Axial flow
Wind tunnel testing
Mathematical analysis
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910713895903321
Beckwith Ivan E.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles Part 2-applications / / P.D. Thomas ; prepared for Langley Research Center
Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles Part 2-applications / / P.D. Thomas ; prepared for Langley Research Center
Autore Thomas P. D (Paul Denis), <1935->
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1980
Descrizione fisica 1 online resource (iv, 113 pages) : illustrations
Collana NASA contractor report
Soggetto topico Jet nozzles
Nozzles - Fluid dynamics
Navier-Stokes equations
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704238703321
Thomas P. D (Paul Denis), <1935->  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface / / by Marvin E. Goldstein and Robert Siegel
Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface / / by Marvin E. Goldstein and Robert Siegel
Autore Goldstein Marvin E.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969
Descrizione fisica 1 online resource (ii, 42 pages) : illustrations
Collana NASA technical note
Soggetto topico Jets - Fluid dynamics
Nozzles - Fluid dynamics
Rockets (Aeronautics) - Nozzles
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910714093303321
Goldstein Marvin E.  
Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui