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.
Advanced noise control fan aerodynamic performance [[electronic resource] /] / Richard F. Bozak, Jr
| Advanced noise control fan aerodynamic performance [[electronic resource] /] / Richard F. Bozak, Jr |
| Autore | Bozak Richard F., Jr. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Noise reduction
Aerodynamic characteristics Inlet pressure Static pressure Flow measurement Flow distribution Mass flow Acoustics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696921303321 |
Bozak Richard F., Jr.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / / David M. Schuster
| Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / / David M. Schuster |
| Autore | Schuster D. M (David M.) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2001 |
| Descrizione fisica | 1 online resource (37 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Transonic wind tunnels
Aerodynamic characteristics Dynamic pressure Static pressure Viscous flow Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706548703321 |
|
Schuster D. M (David M.)
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
An airfoil flutter model suspension system to accommodate large static transonic airloads [[electronic resource] /] / Wilmer H. Reed, III
| An airfoil flutter model suspension system to accommodate large static transonic airloads [[electronic resource] /] / Wilmer H. Reed, III |
| Autore | Reed Wilmer H |
| Pubbl/distr/stampa | Newport News, VA : , : DEI-Tech, Inc. |
| Descrizione fisica | 1 online resource (36 pages) : illustrations |
| Collana |
NASA contractor report
NASA-CR-177998 |
| Soggetto topico |
Airfoils
Blowdown wind tunnels Flutter analysis Pressure distribution Static pressure Supercritical airfoils Transonic wind tunnels Two dimensional flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701788903321 |
|
Reed Wilmer H
|
||
| Newport News, VA : , : DEI-Tech, Inc. | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| ||
Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment / / Donald Greer [and three others]
| Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment / / Donald Greer [and three others] |
| Autore | Greer Donald <1896-> |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Facility, , July 1999 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Airfoils
High altitude Low Reynolds number Navier-Stokes equation Aerodynamic drag Static pressure Subsonic speed Boundary layer stability Flight tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Design and predictions for a high-altitude |
| Record Nr. | UNINA-9910706187803321 |
|
Greer Donald <1896->
|
||
| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Facility, , July 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Effect of sweep on cavity flow fields at subsonic and transonic speeds [[electronic resource] /] / Maureen B. Tracy ... [and others]
| Effect of sweep on cavity flow fields at subsonic and transonic speeds [[electronic resource] /] / Maureen B. Tracy ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (viii, 240 pages) : illustrations (some color) |
| Altri autori (Persone) | TracyMaureen B |
| Collana | NASA/TM |
| Soggetto topico |
Cavity flow
Cavities Flow distribution Leading edge sweep Pressure distribution Sweep angle Trailing edges Static pressure |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702299503321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall
| Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall |
| Autore | Hughes Donald L (Donald Lee), <1926-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static pressure
Aircraft engines Inlet flow Flight tests Pressure measurement Static pressure probes - Testing Airplanes - Turbojet engines - Air intakes Eagle (Jet fighter plane) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709611203321 |
|
Hughes Donald L (Donald Lee), <1926->
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| ||
Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / / Gary E. Erickson
| Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / / Gary E. Erickson |
| Autore | Erickson Gary E. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2013] |
| Descrizione fisica | 1 online resource (50 pages) : illustrations |
| Collana | NASA/TM 2013-217977 |
| Soggetto topico |
Aerodynamic loads
Angle of attack Dynamic pressure Mach number Static pressure Trailing edge flaps Optical measurement Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704753403321 |
|
Erickson Gary E.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / / Hyun D. Kim, Warren R. Hingst, and David O. Davis
| Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / / Hyun D. Kim, Warren R. Hingst, and David O. Davis |
| Autore | Kim Hyun Dae |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Boundary layer control
Pressure measurement Flow visualization Turbulent boundary layer Mass flow rate Static pressure Shock waves |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707497503321 |
|
Kim Hyun Dae
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Soggetto topico
-
Static pressure
(20)
- Wind tunnel tests (7)
- Angle of attack (4)
- Flow distribution (3)
- Mach number (3)