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Delay of transition using forced damping / / Reginald J. Exton
| Delay of transition using forced damping / / Reginald J. Exton |
| Autore | Exton Reginald J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2014 |
| Descrizione fisica | 1 online resource (27 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Leading edges
Boundary layer transition Boundary layer stability Damping Laminar boundary layer |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703731303321 |
Exton Reginald J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Greer Donald <1896->
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Facility, , July 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Feasibility and benefits of laminar flow control on supersonic cruise airplanes [[electronic resource] /] / A.G. Powell, S. Agrawal, T. R. Lacey
| Feasibility and benefits of laminar flow control on supersonic cruise airplanes [[electronic resource] /] / A.G. Powell, S. Agrawal, T. R. Lacey |
| Autore | Powell A. G |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989] |
| Descrizione fisica | 1 volume |
| Altri autori (Persone) |
AgrawalSudhir
LaceyT. R |
| Collana | NASA contractor report |
| Soggetto topico |
Aerodynamic configurations
Boundary layer control Boundary layer stability Feasibility analysis Fighter aircraft Laminar boundary layer Laminar flow Supersonic aircraft Supersonic cruise aircraft research Supersonic transports |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910698995003321 |
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Powell A. G
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wave phenomena in a high Reynolds number compressible boundary layer [[electronic resource] /] / A. Bayliss ... [and others]
| Wave phenomena in a high Reynolds number compressible boundary layer [[electronic resource] /] / A. Bayliss ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, , [1985] |
| Descrizione fisica | 1 volume : PDF file |
| Altri autori (Persone) | BaylissAlvin |
| Collana |
ICASE report
NASA-CR |
| Soggetto topico |
Boundary layer control
Boundary layer stability Compressible flow Reynolds number Viscous flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699206903321 |
| Hampton, Va. : , : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / / Robert L. Stallings, Jr., and Milton Lamb
| Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / / Robert L. Stallings, Jr., and Milton Lamb |
| Autore | Stallings Robert L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (45 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Boundary layer flow
Boundary layer stability Heat transfer Reynolds number Wind tunnel tests Aerothermodynamics Boundary layer Supersonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707438603321 |
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Stallings Robert L.
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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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