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Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet / / René Fernandez [and three others]
Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet / / René Fernandez [and three others]
Autore Fernandez René
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2001
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA/TM
Soggetto topico Scale models
Inlet pressure
Performance tests
Wind tunnel tests
Rocket-based combined-cycle engines
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706600403321
Fernandez René  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Performance optimization of a rotor alone Nacelle for acoustic fan testing / / C.C. Cunningham, W.K. Thompson, and C.E. Hughes
Performance optimization of a rotor alone Nacelle for acoustic fan testing / / C.C. Cunningham, W.K. Thompson, and C.E. Hughes
Autore Cunningham C. C.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000
Descrizione fisica 1 online resource (9 pages) : illustrations
Collana NASA/TM
Soggetto topico Acoustic properties
Automatic control
Error analysis
Nacelles
Rotor speed
Test chambers
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706210803321
Cunningham C. C.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel [[electronic resource] ] : progress report / / William J. Cook and Tim A. Giddings
Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel [[electronic resource] ] : progress report / / William J. Cook and Tim A. Giddings
Autore Cook William John <1929->
Pubbl/distr/stampa Ames, Iowa : , : Engineering Research Institute, Iowa State University, , [1984]
Descrizione fisica 1 online resource (iii, 42 pages) : illustrations
Altri autori (Persone) GiddingsTim A
Collana NASA contractor report
Soggetto topico Boundary layer flow
Flow distribution
Oscillating flow
Performance tests
Steady flow
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel
Record Nr. UNINA-9910700193803321
Cook William John <1929->  
Ames, Iowa : , : Engineering Research Institute, Iowa State University, , [1984]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Potential benefits of magnetic suspension and balance systems [[electronic resource] /] / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore
Potential benefits of magnetic suspension and balance systems [[electronic resource] /] / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore
Autore Lawing Pierce L
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987]
Descrizione fisica 1 volume
Altri autori (Persone) DressDavid A
KilgoreRobert A
Collana NASA technical memorandum
Soggetto topico Aerodynamic balance
Aerodynamic coefficients
Aerodynamic stability
Magnetic suspension
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910698894603321
Lawing Pierce L  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Quantitative global heat transfer in a Mach-6 quiet tunnel / / John P. Sullivan [and ten others]
Quantitative global heat transfer in a Mach-6 quiet tunnel / / John P. Sullivan [and ten others]
Autore Sullivan John P.
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Descrizione fisica 1 online resource (148 pages) : color illustrations
Collana [NASA contractor report]
Soggetto topico Heat transfer
Hypersonic speed
Temperature sensitive paints
Wind tunnel tests
Hypersonic wind tunnels
Heat flux
Mathematical models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702091603321
Sullivan John P.  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin
Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin
Autore Marroquin J.
Pubbl/distr/stampa Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Descrizione fisica 1 online resource (iii, 27 pages) : illustrations
Collana NASA/CR
Soggetto topico Aerothermodynamics
Hypersonic heat transfer
Aerodynamic heat transfer
Hypersonic speed
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel
Record Nr. UNINA-9910709972703321
Marroquin J.  
Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) / / J. Marroquin
Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) / / J. Marroquin
Autore Marroquin J.
Pubbl/distr/stampa Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Descrizione fisica 1 online resource (iv, 164 pages) : illustrations
Collana NASA/CR
Soggetto topico Wind tunnel tests
Aerodynamic heating
External tanks
Space shuttles
Mach number
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility
Record Nr. UNINA-9910709972903321
Marroquin J.  
Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Results of an experimental program investigating the effects of simulated ice on the performance of the NACA 63A415 airfoil with flap / / R.J. Zaguli, M.B. Bragg, and G.M. Gregorek
Results of an experimental program investigating the effects of simulated ice on the performance of the NACA 63A415 airfoil with flap / / R.J. Zaguli, M.B. Bragg, and G.M. Gregorek
Autore Zaguli R. J.
Pubbl/distr/stampa [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1984
Descrizione fisica 1 online resource (iii, 179 pages) : illustrations
Collana NASA/CR
Soggetto topico Glazes
Airfoils
Ice formation
Wind tunnel tests
Flow visualization
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709694803321
Zaguli R. J.  
[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) / / J. Marroquin and R.B. Kingsland
Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) / / J. Marroquin and R.B. Kingsland
Autore Marroquin J.
Pubbl/distr/stampa Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Descrizione fisica 1 online resource (iii, 113 pages) : illustrations
Collana NASA/CR
Soggetto topico Fluid flow
Failure analysis
Wind tunnel tests
Flow distribution
Subsonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center
Record Nr. UNINA-9910709972803321
Marroquin J.  
Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Review of blunt body wake flows at hypersonic low density conditions / / J.N. Moss and J.M. Price
Review of blunt body wake flows at hypersonic low density conditions / / J.N. Moss and J.M. Price
Autore Moss James N.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1996]
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA-TM
Soggetto topico Wakes
Hypersonic flow
Blunt bodies
Rarefaction
Nose cones
Wind tunnel tests
Flow distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705772803321
Moss James N.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, , [1996]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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