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Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel / / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui
| Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel / / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui |
| Autore | Wilcox Floyd J., Jr. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (45 pages) : illustrations (some color) |
| Collana | NASA/TP |
| Soggetto topico |
Angle of attack
Mach number Pressure measurement Sonic booms Wind tunnels Wedges |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705480803321 |
Wilcox Floyd J., Jr.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013 | ||
| 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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Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers / / Patrick C. Stoliker and John T. Bosworth
| Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers / / Patrick C. Stoliker and John T. Bosworth |
| Autore | Stoliker P. C. |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 1996 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aircraft maneuvers
Angle of attack Flight control Pilot induced oscillation X-31 aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707009503321 |
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Stoliker P. C.
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of icing scaling on swept NACA 0012 airfoil models / / Jen-Ching Tsao, Sam Lee
| Evaluation of icing scaling on swept NACA 0012 airfoil models / / Jen-Ching Tsao, Sam Lee |
| Autore | Tsao Jen-Ching |
| Pubbl/distr/stampa | Brook Park, Ohio : , : Ohio Aerospace Institute |
| Descrizione fisica | 1 online resource (16 pages) : color illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Ice formation
Scale models Angle of attack Aircraft icing Convective heat transfer Heat transfer coefficients Stagnation point Sweep angle |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702111303321 |
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Tsao Jen-Ching
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| Brook Park, Ohio : , : Ohio Aerospace Institute | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / / Jimmy L. Pittman and Gregory D. Riebe
| Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / / Jimmy L. Pittman and Gregory D. Riebe |
| Autore | Pittman Jimmy L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (113 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Aerodynamic characteristics
Aerodynamic configurations Angle of attack Hypersonic aircraft Supersonic aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707455703321 |
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Pittman Jimmy 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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Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack
| Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack |
| Autore | Mack Robert J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Nacelles
Ducted flow Mach number Ducted bodies Flow characteristics Fluid flow Angle of attack Aircraft design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705868803321 |
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Mack Robert J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental effects of wing location on wing-body pressures at supersonic speeds / / Jerry M. Allen and Carolyn B. Watson
| Experimental effects of wing location on wing-body pressures at supersonic speeds / / Jerry M. Allen and Carolyn B. Watson |
| Autore | Allen Jerry M. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1993 |
| Descrizione fisica | 1 online resource (195 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Angle of attack
Body-wing configurations Flow coefficients Pressure distribution Supersonic flight Supersonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707953503321 |
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Allen Jerry M.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / / Gary E. Erickson
| Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / / 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 (50 pages) : illustrations |
| Collana | NASA/TM 2013-217977 |
| Soggetto topico |
Aerodynamic loads
Angle of attack Dynamic pressure Mach number Static pressure Trailing edge flaps Optical measurement Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704753403321 |
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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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Experimental measurements of sonic boom signatures using a continuous data acquistion technique / / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui
| Experimental measurements of sonic boom signatures using a continuous data acquistion technique / / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui |
| Autore | Wilcox Floyd J (Floyd Jay) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (45 pages) : illustrations (some color) |
| Collana | NASA/TP |
| Soggetto topico |
Angle of attack
Data acquisition Information flow Mach number Reynolds number Sonic booms Wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705468003321 |
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Wilcox Floyd J (Floyd Jay)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / / Floyd J. Wilcox, Jr. [and five others]
| Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / / Floyd J. Wilcox, Jr. [and five others] |
| Autore | Wilcox Floyd J (Floyd Jay) |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (130 pages) : illustrations |
| Collana | [NASA technical memorandum] |
| Soggetto topico |
Sonic booms
Wind tunnel tests Supersonic speed Angle of attack |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702349803321 |
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Wilcox Floyd J (Floyd Jay)
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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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Soggetto topico
-
Angle of attack
(46)
- Mach number (9)
- Wind tunnel tests (9)
- Aerodynamic characteristics (7)
- F-18 aircraft (7)