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.
Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009
Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009
Autore Slater John W
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (27 pages) : illustrations
Altri autori (Persone) SaundersJohn D
Collana NASA/TM
Soggetto topico Computational fluid dynamics 241
Data simulation
Hypersonics
Static pressure
Supersonic combustion ramjet engines
Wind tunnel tests
Aerodynamics
Boundary layers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Computational fluid dynamics
Record Nr. UNINA-9910699653003321
Slater John W  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Design and analysis tool for external-compression supersonic inlets [[electronic resource] /] / John W. Slater
Design and analysis tool for external-compression supersonic inlets [[electronic resource] /] / John W. Slater
Autore Slater John W
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (23 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Supersonic inlets
Flow distribution
Aerodynamic characteristics
Drag
Flow velocity
Supersonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702353503321
Slater John W  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Planar Inlet Design and Analysis Process (PINDAP) [[electronic resource] /] / John W. Slater, Christopher R. Gruber
Planar Inlet Design and Analysis Process (PINDAP) [[electronic resource] /] / John W. Slater, Christopher R. Gruber
Autore Slater John W
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Descrizione fisica 1 online resource (10 pages) : illustrations (some color)
Altri autori (Persone) GruberChristopher R
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Hypersonic inlets
Supersonic inlets
Planar structures
Engine design
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Planar Inlet Design and Analysis Process
Record Nr. UNINA-9910701473403321
Slater John W  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui