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High-temperature modal survey of a hot-structure control surface [[electronic resource] /] / Natalie D. Spivey
| High-temperature modal survey of a hot-structure control surface [[electronic resource] /] / Natalie D. Spivey |
| Autore | Spivey Natalie D |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] |
| Descrizione fisica | 1 online resource (26 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Control surfaces
High temperature Wind tunnel tests Fabrication Vibration tests Carbon-silicon carbide composites X-37 vehicle |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701851303321 |
Spivey Natalie D
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| Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes / / Daniel L. Sutliff and Clifford A. Brown, Bruce E. Walker
| Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes / / Daniel L. Sutliff and Clifford A. Brown, Bruce E. Walker |
| Autore | Sutliff Daniel L (Daniel Linden), <1962-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014 |
| Descrizione fisica | 1 online resource (44 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Acoustic properties
Aerodynamic configurations Turbofan engines Ducts Aerodynamic noise Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702440003321 |
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Sutliff Daniel L (Daniel Linden), <1962->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Icing Research Tunnel (IRT) Force Measurement System (FMS) / / Paul W. Roberts
| Icing Research Tunnel (IRT) Force Measurement System (FMS) / / Paul W. Roberts |
| Autore | Roberts Paul W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (68 pages) : illustrations |
| Collana | NASA/TM 2012-217784 |
| Soggetto topico |
Ice formation
Aerodynamic characteristics Design analysis Systems analysis Wind tunnel tests Test facilities |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Icing Research Tunnel |
| Record Nr. | UNINA-9910704474603321 |
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Roberts Paul W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Improvements to the total temperature calibration of the NASA Glenn Icing Research Tunnel [[electronic resource] /] / E. Allen Arrington and Jose C. Gonsalez ; prepared for the 41st Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Tucson, Arizona, July 10-13, 2005
| Improvements to the total temperature calibration of the NASA Glenn Icing Research Tunnel [[electronic resource] /] / E. Allen Arrington and Jose C. Gonsalez ; prepared for the 41st Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Tucson, Arizona, July 10-13, 2005 |
| Autore | Arrington E. Allen |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] |
| Descrizione fisica | 1 online resource (59 pages) : color illustrations |
| Altri autori (Persone) | GonsalezJose C |
| Collana | NASA/CR |
| Soggetto topico |
Ice formation
Research facilities Wind tunnel tests Calibrating Temperature measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701386403321 |
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Arrington E. Allen
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel [[electronic resource] /] / David M. Elliott
| Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel [[electronic resource] /] / David M. Elliott |
| Autore | Elliott David M |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (22 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Wind tunnel tests
Rotor aerodynamics Low speed wind tunnels Rotor blades (turbomachinery) Counter rotation Scale models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701916803321 |
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Elliott David M
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter
| An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter |
| Autore | Arbiter Dorothy G |
| Pubbl/distr/stampa | Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] |
| Descrizione fisica | 1 volume : PDF file |
| Collana | NASA contractor report |
| Soggetto topico |
Axisymmetric bodies
Investigation Nozzle thrust coefficients Ports (openings) Rotating cylinders Static tests Thrust reversal Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699288403321 |
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Arbiter Dorothy G
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| Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / / by Mary W. Jackson and K.R. Czarnecki
| Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / / by Mary W. Jackson and K.R. Czarnecki |
| Autore | Jackson Mary W. |
| Pubbl/distr/stampa | Washington : , : National Aeronautics and Space Administration, , April 1960 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Reynolds number
Turbulence Conical bodies Supersonic boundary layers Surface roughness effects Transition points Turbulent boundary layer Turbulent flow Wind tunnel tests Schlieren photography Supersonic speed Wind tunnel models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715362303321 |
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Jackson Mary W.
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| Washington : , : National Aeronautics and Space Administration, , April 1960 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests / / Alonzo L. Frost and Charlie C. Dill
| Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests / / Alonzo L. Frost and Charlie C. Dill |
| Autore | Frost Alonzo L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1986 |
| Descrizione fisica | 1 online resource (vi, 175 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Computerized simulation
Plumes Wind tunnel tests Space shuttles Base pressure Space shuttles - Propulsion systems - Testing Plumes (Fluid dynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910693055803321 |
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Frost Alonzo L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An investigation of the causes of failure of flexible thermal protection materials in an aerodynamic environment / / Charles F. Coe
| An investigation of the causes of failure of flexible thermal protection materials in an aerodynamic environment / / Charles F. Coe |
| Autore | Coe Charles F. |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Ames Research Center, , March 1987 |
| Descrizione fisica | 1 online resource (i, 29 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Failure analysis
Thermal protection Dynamic pressure Wind tunnel tests Shock waves |
| Soggetto genere / forma | Online resources. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709874503321 |
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Coe Charles F.
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| Edwards, California : , : National Aeronautics and Space Administration, Ames Research Center, , March 1987 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments / / David M. Schuster [and ten others]
| Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments / / David M. Schuster [and ten others] |
| Autore | Schuster D. M (David M.) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016 |
| Descrizione fisica | 1 online resource (97 pages) : color illustrations. |
| Collana | NASA/TM |
| Soggetto topico |
Buffeting
Dynamic loads Launch vehicles Pressure sensitive paints Spacecraft launching Unsteady flow Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Investigation of unsteady pressure-sensitive paint |
| Record Nr. | UNINA-9910707921103321 |
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Schuster D. M (David M.)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Wind tunnel tests
(154)
- Aerodynamic characteristics (20)
- Flow distribution (16)
- Ice formation (15)
- Computational fluid dynamics (13)