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Application of background oriented Schlieren for altitude testing of rocket engines / / Mark P. Wernet, Benjamin R. Stiegemeier
Application of background oriented Schlieren for altitude testing of rocket engines / / Mark P. Wernet, Benjamin R. Stiegemeier
Autore Wernet Mark P.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2017
Descrizione fisica 1 online resource (10 pages) : color illustrations
Collana NASA/TM
Soggetto topico Flow visualization
Altitude tests
Schlieren photography
Shadowgraph photography
Rocket exhaust
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706511703321
Wernet Mark P.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop / / Vance F. Dippold, III
Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop / / Vance F. Dippold, III
Autore Dippold Vance
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014
Descrizione fisica 1 online resource (18 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Convergent nozzles
Navier-Stokes equation
Reynolds averaging
Shadowgraph photography
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703624903321
Dippold Vance  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / / K. Yamamoto [and four others]
Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / / K. Yamamoto [and four others]
Autore Yamamoto K.
Pubbl/distr/stampa Cincinnati, Ohio : , : General Electric Company, Aircraft Engine Business Group, , February, 1984
Descrizione fisica 1 online resource (2 volumes) : illustrations
Collana NASA CR
Soggetto topico Acoustic measurement
Nozzle design
Scale models
Laser doppler velocimeters
Shadowgraph photography
Static pressure
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto v. 1. Test nozzles and acoustic data -- v. 2. Laser velocimeter data, static pressures and shadowgraph photos.
Altri titoli varianti Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight
Record Nr. UNINA-9910703872603321
Yamamoto K.  
Cincinnati, Ohio : , : General Electric Company, Aircraft Engine Business Group, , February, 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui