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Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt
| Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt |
| Autore | Nowak Robert J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 |
| Descrizione fisica | 1 online resource (87 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Flow distribution
Cones Aerodynamic heating Boundary layer transition Turbulent boundary layer Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number Aerothermodynamics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709616703321 |
Nowak Robert J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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COSAL : a black-box compressible stability analysis code for transition prediction in three-dimensional boundary layers / / Mujeeb R. Malik
| COSAL : a black-box compressible stability analysis code for transition prediction in three-dimensional boundary layers / / Mujeeb R. Malik |
| Autore | Malik Mujeeb R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1982 |
| Descrizione fisica | 1 online resource (ii, 226 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Compressible boundary layer
Aircraft design Swept wings Boundary layer transition Three dimensional boundary layer |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | COSAL |
| Record Nr. | UNINA-9910709640703321 |
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Malik Mujeeb R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1982 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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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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Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition [[electronic resource] /] / Rudolph A. King, Scott A. Berry, Michael A. Kegerise
| Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition [[electronic resource] /] / Rudolph A. King, Scott A. Berry, Michael A. Kegerise |
| Autore | King Rudolph A |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2008] |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Altri autori (Persone) |
BerryScott A
KegeriseMichael A |
| Collana | NASA TM- |
| Soggetto topico |
Boundary layer transition
Hypersonics Protuberances Space Shuttle orbiters Thermography Shapes Heat transfer |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699550403321 |
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King Rudolph A
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2008] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / / Brian R. Hollis
| Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / / Brian R. Hollis |
| Autore | Hollis Brian R (Brian Ray) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017 |
| Descrizione fisica | 1 online resource (viii, 168 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layer transition
Hypersonic wind tunnels Surface roughness Surface roughness effects Thermography |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705705303321 |
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Hollis Brian R (Brian Ray)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages [[electronic resource] /] / Wang Tie-cheng
| An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages [[electronic resource] /] / Wang Tie-cheng |
| Autore | Wang Tiecheng |
| Pubbl/distr/stampa | Washington DC : , : National Aeronautics and Space Administration, , [1986] |
| Descrizione fisica | 1 online resource (8 pages) |
| Collana | NASA technical memorandum |
| Soggetto topico |
Airfoils
Boundary layer transition Hot-film anemometers Turbulent boundary layer Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700854803321 |
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Wang Tiecheng
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| Washington DC : , : National Aeronautics and Space Administration, , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental study of boundary layer behavior in a simulated low pressure turbine / / Rickey J. Shyne
| Experimental study of boundary layer behavior in a simulated low pressure turbine / / Rickey J. Shyne |
| Autore | Shyne Rickey J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , October 1998 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Fluid dynamics
Flow visualization Low pressure Turbines Boundary layer separation Turbulent flow Boundary layer transition Turbulent boundary layer Wind tunnel tests Flow measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705831803321 |
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Shyne Rickey J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , October 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight tests of a supersonic natural laminar flow airfoil / / Michael A. Frederick [and three others]
| Flight tests of a supersonic natural laminar flow airfoil / / Michael A. Frederick [and three others] |
| Autore | Frederick Michael A. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , December 2015 |
| Descrizione fisica | 1 online resource (29 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layer transition
Chords (geometry) Laminar flow Leading edge sweep Supersonic airfoils |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707069903321 |
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Frederick Michael A.
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| Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , December 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight-measured laminar boundary layer transition phenomena including stability theory analysis / / Clifford J. Obara and Bruce J. Holmes
| Flight-measured laminar boundary layer transition phenomena including stability theory analysis / / Clifford J. Obara and Bruce J. Holmes |
| Autore | Obara Clifford J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1985 |
| Descrizione fisica | 1 online resource (37 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Boundary layer transition
Aerodynamic coefficients Laminar flow Turbulent boundary layer Flight tests Boundary layer Transition flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709796403321 |
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Obara Clifford J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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HyBoLT flight experiment [[electronic resource] /] / Fang-Jenq (Frank) Chen and Scott A. Berry
| HyBoLT flight experiment [[electronic resource] /] / Fang-Jenq (Frank) Chen and Scott A. Berry |
| Autore | Chen Fang-Jenq |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] |
| Descrizione fisica | 1 online resource (iii, 71 pages) : illustrations |
| Altri autori (Persone) | BerryScott A |
| Collana | NASA/TM- |
| Soggetto topico |
HyBoLT flight experiment
Aeronautical engineering Hypersonic boundary layer Transition flight Flight control Boundary layer transition |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699647303321 |
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Chen Fang-Jenq
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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