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Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven others]
| Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven others] |
| Autore | Campbell Bryan A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (128 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layer control
Leading edges Wind tunnel tests Flaps (control surfaces) Pressure effects Subsonic speed Supersonic transports Aerodynamic configurations |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration |
| Record Nr. | UNINA-9910706520903321 |
Campbell Bryan A.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber / / S. Naomi McMillin [and five others]
| Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber / / S. Naomi McMillin [and five others] |
| Autore | McMillin S. Naomi (Susan Naomi) |
| Pubbl/distr/stampa | Hampton, VA : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996 |
| Descrizione fisica | 1 online resource (iii, 262 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Delta wings
Flow visualization Leading edges Reynolds number Boundary layer transition |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704382503321 |
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McMillin S. Naomi (Susan Naomi)
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| Hampton, VA : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A thermostructural analysis of a diboride composite leading edge / / Tom Kowalski [and three others]
| A thermostructural analysis of a diboride composite leading edge / / Tom Kowalski [and three others] |
| Autore | Kowalski Tom |
| Pubbl/distr/stampa | Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , July 1996 |
| Descrizione fisica |
viii, 43 pages : illustrations
1 online resource (29 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Leading edges
Aerothermodynamics Finite element method Composite materials Tensile stress Aerodynamic heating Thermodynamic properties Compressive strength Structural analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910708067803321 |
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Kowalski Tom
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| Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , July 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge [[electronic resource] /] / Sandra P. Walker and Jerry E. Warren
| Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge [[electronic resource] /] / Sandra P. Walker and Jerry E. Warren |
| Autore | Walker Sandra P |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (some color) |
| Altri autori (Persone) | WarrenJerry E |
| Collana | NASA/TM |
| Soggetto topico |
Leading edges
Mathematical models Space Shuttle orbiters Wing panels Spallation Coatings Carbon-carbon composites Thermodynamic properties |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702004103321 |
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Walker Sandra P
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Turbulent wing-leading-edge correlation assessment for the shuttle orbiter [[electronic resource] /] / Rudolph A. King and Matthew P. Vaughan
| Turbulent wing-leading-edge correlation assessment for the shuttle orbiter [[electronic resource] /] / Rudolph A. King and Matthew P. Vaughan |
| Autore | King Rudolph A |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2009] |
| Descrizione fisica | 1 online resource (33 unnumbered pages) : illustrations |
| Altri autori (Persone) | VaughanMatthew P |
| Collana | NASA TM- |
| Soggetto topico |
Space Shuttle orbiters
Boundary layers Turbulent boundary layer Space transportation system Damage assessment Leading edges Reentry trajectories Contaminants |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696908103321 |
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King Rudolph A
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Ultra high temperature (UHT) SiC fiber (phase II) / / James A. DiCarlo [and three others]
| Ultra high temperature (UHT) SiC fiber (phase II) / / James A. DiCarlo [and three others] |
| Autore | DiCarlo James A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2015 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Silicon carbides
Ceramic matrix composites Hypersonic vehicles Gas turbine engines Leading edges |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Ultra high temperature |
| Record Nr. | UNINA-9910704272903321 |
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DiCarlo James A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields [[electronic resource] /] / Gary E. Erickson
| Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields [[electronic resource] /] / Gary E. Erickson |
| Autore | Erickson Gary E |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] |
| Descrizione fisica | 1 online resource (v, 32 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Aerodynamic configurations
Pressure sensitive paints Flow visualization Shock waves Static pressure Leading edges Angle of attack |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697041803321 |
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Erickson Gary E
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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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Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program / / Robert W. Moses
| Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program / / Robert W. Moses |
| Autore | Moses Robert W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1997 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Piezoelectricity
Buffeting Active control Tail assemblies Supersonic aircraft Vortices Angle of attack Aeroelasticity Leading edges Root-mean-square errors |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Vertical tail buffeting alleviation using piezoelectric actuators |
| Record Nr. | UNINA-9910708070703321 |
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Moses Robert W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds / / Gary E. Erickson
| Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds / / 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 (521 pages) : illustrations |
| Collana | NASA/TM 2013-217982 |
| Soggetto topico |
Leading edges
Aerodynamic configurations Angle of attack Canard configurations Flow visualization Subsonic speed Porosity Transonic speed Vortices Reynolds number Mach number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704753303321 |
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Erickson Gary E.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Leading edges
(29)
- Aerodynamic configurations (5)
- Airfoils (5)
- Flow visualization (5)
- Angle of attack (4)