top

  Info

  • Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.

  Info

  • Utilizzare questo link per rimuovere la selezione effettuata.
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / / Milo D. Dahl
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / / Milo D. Dahl
Autore Dahl Milo D. <1956->
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996
Descrizione fisica 1 online resource (21 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Supersonic jet flow
Ducts
Ducted flow
Duct geometry
Circles (geometry)
Boundary conditions
Kelvin-Helmholtz instability
Supersonic inlets
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707311303321
Dahl Milo D. <1956->  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack
Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack
Autore Mack Robert J.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998
Descrizione fisica 1 online resource (20 pages) : illustrations
Collana NASA/TM
Soggetto topico Nacelles
Ducted flow
Mach number
Ducted bodies
Flow characteristics
Fluid flow
Angle of attack
Aircraft design
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705868803321
Mack Robert J.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length / / C.R. Wang [and three others]
Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length / / C.R. Wang [and three others]
Autore Wang C. R.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , May 1997
Descrizione fisica 1 online resource (19 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Heat transfer
Turbines
Navier-Stokes equation
Heat transfer coefficients
Flow characteristics
Ducted flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707608703321
Wang C. R.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , May 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer [[electronic resource] ] : final report / / R. A. Crawford ... [and others]
Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer [[electronic resource] ] : final report / / R. A. Crawford ... [and others]
Pubbl/distr/stampa Tullahoma, Tenn. : , : University of Tennessee Space Institute
Descrizione fisica 1 online resource (51 pages, 135 unnumbered pages) : illustrations
Altri autori (Persone) CrawfordR. A
Collana NASA contractor report
Soggetto topico Computational fluid dynamics
Ducted flow
Incompressible flow
Reynolds number
Three dimensional boundary layer
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer
Record Nr. UNINA-9910701729203321
Tullahoma, Tenn. : , : University of Tennessee Space Institute
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A survey of oscillating flow in Stirling engine heat exchangers [[electronic resource] /] / Terrence W. Simon and Jorge R. Seume
A survey of oscillating flow in Stirling engine heat exchangers [[electronic resource] /] / Terrence W. Simon and Jorge R. Seume
Autore Simon T. W
Pubbl/distr/stampa [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1988]
Descrizione fisica 1 volume
Altri autori (Persone) SeumeJorge R
Collana NASA contractor report
Soggetto topico Ducted flow
Heat exchangers
Oscillating flow
Parameter identification
Stirling engines
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910698990603321
Simon T. W  
[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1988]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow / / Kenneth J. Baumeister and Kevin L. Kreider
Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow / / Kenneth J. Baumeister and Kevin L. Kreider
Autore Baumeister Kenneth J.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Finite difference theory
Sound propagation
Aircraft engines
Aeroacoustics
Real time operation
Engine inlets
Ducted flow
Iterative solution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707310803321
Baumeister Kenneth J.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui