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Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2 / / Gustavo Fujiwara [and ten others]
| Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2 / / Gustavo Fujiwara [and ten others] |
| Autore | Fujiwara Gustavo |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2017 |
| Descrizione fisica | 1 online resource (vi, 112 pages) : illustrations (mostly color) |
| Collana | NASA CR |
| Soggetto topico |
Ice formation
Aircraft icing Aerodynamics Simulation Wind tunnel tests |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Development of experimental icing simulation capability for full-scale swept wings |
| Record Nr. | UNINA-9910708610003321 |
Fujiwara Gustavo
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking / / Sam Lee, Billy Barnhart, Thomas P. Ratvasky
| Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking / / Sam Lee, Billy Barnhart, Thomas P. Ratvasky |
| Autore | Lee Sam |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Stirling cycle
Wind tunnel tests Ice formation Ice prevention Thermal protection Aerodynamic stalling Low Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702487803321 |
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Lee Sam
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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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Effectiveness of micro-blowing technique in adverse pressure gradients / / Gerard E. Welch [and three others]
| Effectiveness of micro-blowing technique in adverse pressure gradients / / Gerard E. Welch [and three others] |
| Autore | Welch Gerard E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center : , : U.S. Army Research Laboratory, , January 2001 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana |
NASA/TM
ARL-TR |
| Soggetto topico |
Blowing
Skin friction Drag reduction Wind tunnel tests Pressure gradients Turbulent flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706572803321 |
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Welch Gerard E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center : , : U.S. Army Research Laboratory, , January 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Yetter Jeffery A.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam
| Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam |
| Autore | Putnam Lawrence E (Lawrence Elwood) |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (67 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerodynamic characteristics
Transonic speed Wind tunnel tests Nacelles Transport aircraft Airplanes - Nacelles Transport planes - Design and construction Stability of airplanes, Longitudinal |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709713903321 |
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Putnam Lawrence E (Lawrence Elwood)
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Estimated benefits of variable-geometry wing camber control for transport aircraft / / Alexander Bolonkin, Glenn B. Gilyard
| Estimated benefits of variable-geometry wing camber control for transport aircraft / / Alexander Bolonkin, Glenn B. Gilyard |
| Autore | Bolonkin Alexander |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , October 1999 |
| Descrizione fisica | 1 online resource (v, 40 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Wing camber
Wind tunnel tests Transport aircraft Adaptive control Cambered wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706186803321 |
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Bolonkin Alexander
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , October 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Estimates for the aerodynamic coefficients of ringsail and disk-gap-band parachutes operating on Mars / / Juan R. Cruz and Miranda L. Snyder
| Estimates for the aerodynamic coefficients of ringsail and disk-gap-band parachutes operating on Mars / / Juan R. Cruz and Miranda L. Snyder |
| Autore | Cross John R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2017 |
| Descrizione fisica | 1 online resource (xii, 101 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Wind tunnel tests
Aerodynamic coefficients Parachutes Angle of attack Polynomials |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706513003321 |
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Cross John R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Estimation of aircraft nonlinear unsteady parameters from wind tunnel data / / Vladislav Klein, Patrick C. Murphy
| Estimation of aircraft nonlinear unsteady parameters from wind tunnel data / / Vladislav Klein, Patrick C. Murphy |
| Autore | Klein Vladislav |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1998 |
| Descrizione fisica | 1 online resource (38 pages) : illustrations |
| Collana | NASA TM |
| Soggetto topico |
Wind tunnel tests
Unsteady aerodynamics Aerodynamic forces Mathematical models Aircraft stability Flight stability tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706191403321 |
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Klein Vladislav
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny
| Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny |
| Autore | Thomas Scott R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Ejectors
Hydrocarbon fuels Wind tunnel tests Supersonic speed Mach number Engine tests Propulsion system performance Flow distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707625903321 |
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Thomas Scott R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts [[electronic resource] /] / Robert J. Mack
| An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts [[electronic resource] /] / Robert J. Mack |
| Autore | Mack Robert J |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] |
| Descrizione fisica | 1 online resource (24 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Sonic booms
Flow distribution Design analysis Nacelles Interference lift Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697004603321 |
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Mack Robert J
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] | ||
| 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)