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Characterization of Chevron nozzle performance / / Mark P. Wernet and James E. Bridges
Characterization of Chevron nozzle performance / / Mark P. Wernet and James E. Bridges
Autore Wernet Mark P.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2021
Descrizione fisica 1 online resource (27 pages) : illustrations (chiefly color)
Collana NASA/TM
Soggetto topico Particle image velocimetry
Aeroacoustics
Nozzle design
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910716955903321
Wernet Mark P.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2021
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]
Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]
Autore Jones Daniel S.
Pubbl/distr/stampa Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014
Descrizione fisica 1 online resource (25 pages) : color illustrations
Collana NASA/TM
Soggetto topico Convergent-divergent nozzles
Flow distribution
Inviscid flow
Nozzle design
Rocket nozzles
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703728303321
Jones Daniel S.  
Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Development of improved throat inserts for ablative rocket engines / / by Jerry M. Winter and Donald A. Peterson
Development of improved throat inserts for ablative rocket engines / / by Jerry M. Winter and Donald A. Peterson
Autore Winter Jerry M.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , July 1969
Descrizione fisica 1 online resource (ii, 161 pages) : illustrations (some color)
Collana NASA/TN
Soggetto topico Rocket engines
Nozzle design
Ablative materials
Rockets (Aeronautics) - Fuel
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910716079703321
Winter Jerry M.  
Washington, D.C. : , : National Aeronautics and Space Administration, , July 1969
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt
Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt
Autore Yetter Jeffery A.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Descrizione fisica 1 online resource (116 pages) : illustrations
Collana NASA technical paper
Soggetto topico Convergent-divergent nozzles
Exhaust flow simulation
Nozzle design
Static pressure
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707455003321
Yetter Jeffery A.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
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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
Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application [[electronic resource] ] : dual stream nozzles : comprehensive data report / / B.A. Janardan, J.F. Brausch, and A.O. Price
Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application [[electronic resource] ] : dual stream nozzles : comprehensive data report / / B.A. Janardan, J.F. Brausch, and A.O. Price
Autore Janardan B. A
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , [1984]
Descrizione fisica 1 online resource (501 unnumbered pages) : illustrations
Altri autori (Persone) BrauschJ. F
PriceA. O
Collana NASA CR
Soggetto topico Acoustic measurement
Aerodynamic forces
Feasibility analysis
Geometry
Heat shielding
Jet aircraft noise
Nozzle design
Suppressors
Variable cycle engines
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Vol. 1 Test nozzles and acoustic data
Altri titoli varianti Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application
Record Nr. UNINA-9910700819103321
Janardan B. A  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , [1984]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / / Bobby L. Berrier and Richard J. Re
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / / Bobby L. Berrier and Richard J. Re
Autore Berrier Bobby L.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Descrizione fisica 1 online resource (215 pages) : chiefly illustrations
Collana NASA technical paper
Soggetto topico Convergent-divergent nozzles
Mach number
Nozzle design
Performance tests
Pressure ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707455903321
Berrier Bobby L.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / / M. Moin Hussaini and John J. Korte
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / / M. Moin Hussaini and John J. Korte
Autore Hussaini M. Moin
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996
Descrizione fisica 1 online resource (12 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Computational fluid dynamics
Navier-Stokes equation
Nozzle design
Rocket nozzles
Low Reynolds number
Nozzle thrust coefficients
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Investigation of low Reynolds number rocket nozzle design using parabolized Navier-Stokes based optimization procedure
Record Nr. UNINA-9910707911603321
Hussaini M. Moin  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Lessons learned during TBCC design for the NASA-AFRL joint system study / / Christopher A. Snyder, A.M. (Jose) Espinosa
Lessons learned during TBCC design for the NASA-AFRL joint system study / / Christopher A. Snyder, A.M. (Jose) Espinosa
Autore Snyder Christopher A.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Descrizione fisica 1 online resource (13 pages) : color illustrations
Collana NASA/TM
Soggetto topico Spacecraft propulsion
Gas turbine engines
Inlet nozzles
Nozzle design
Hypersonic vehicles
Reusable launch vehicles
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Lessons learned during Turbine Based Combined Cycle design for the NASA Air Force Research Laboratory joint system study
Record Nr. UNINA-9910702508403321
Snyder Christopher A.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Multidisciplinary approach to aerospike nozzle design / / J.J. Korte [and six others]
Multidisciplinary approach to aerospike nozzle design / / J.J. Korte [and six others]
Autore Korte J. J.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Nozzle design
Engine design
Multidisciplinary design optimization
Finite element method
Rocket nozzles
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707903703321
Korte J. J.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione