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Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel / / Andy P. Broeren, James T. Riley
| Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel / / Andy P. Broeren, James T. Riley |
| Autore | Broeren Andy P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (34 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Wind tunnel tests
Deicing Fluid flow Boeing 737 aircraft Aerodynamic characteristics Propulsion Flight tests Aircraft icing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704469903321 |
Broeren Andy P.
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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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Role of computational fluid dynamics and wind tunnels in aeronautics R&D / / edited by Mujeeb R. Malik and Dennis M. Bushnell
| Role of computational fluid dynamics and wind tunnels in aeronautics R&D / / edited by Mujeeb R. Malik and Dennis M. Bushnell |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 |
| Descrizione fisica | 1 online resource (vii, 63 pages) : illustrations (some color) |
| Collana | NASA/TP |
| Soggetto topico |
Computational fluid dynamics
Aeronautics Wind tunnel tests Aircraft design Aerospace vehicles Turbulence models Research and development |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704440203321 |
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic acceptance test / / Andy P. Broeren, James T. Riley
| Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic acceptance test / / Andy P. Broeren, James T. Riley |
| Autore | Broeren Andy P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (23 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Lift
Wind tunnel tests Degradation Aircraft icing Fluids Boeing 737 aircraft Flight tests Deicers Aerodynamic configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702486503321 |
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Broeren Andy P.
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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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Shock generation and control using DBD plasma actuators : SBIR phase I final report / / by Mehul P. Patel [and four others]
| Shock generation and control using DBD plasma actuators : SBIR phase I final report / / by Mehul P. Patel [and four others] |
| Autore | Patel Mehul P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (34 pages) : color illustrations |
| Collana | [NASA contractor report] |
| Soggetto topico |
Actuators
Dielectrics Shock tests Wind tunnel tests Aircraft engines Turbulent boundary layer Boundary layer separation Supersonic inlets Oblique shock waves |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Shock generation and control using DBD plasma actuators |
| Record Nr. | UNINA-9910702110403321 |
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Patel Mehul P.
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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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Space shuttle afterbody aerodynamics/plume simulation data summary / / Kenneth L. Blackwell and Leroy M. Hair
| Space shuttle afterbody aerodynamics/plume simulation data summary / / Kenneth L. Blackwell and Leroy M. Hair |
| Autore | Blackwell Kenneth L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , December 1978 |
| Descrizione fisica | 1 online resource (xi, 183 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Aerodynamic characteristics
Aerodynamic configurations Parameterization Space shuttles Wind tunnel tests Plumes (Fluid dynamics) Reusable space vehicles Wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Space shuttle afterbody aerodynamics plume simulation data summary |
| Record Nr. | UNINA-9910707493003321 |
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Blackwell Kenneth L.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , December 1978 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Space shuttle orbiter trimmed center-of-gravity extension study . Volume ix Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 / / W. Pelham Phillips and Roger H. Fournier
| Space shuttle orbiter trimmed center-of-gravity extension study . Volume ix Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 / / W. Pelham Phillips and Roger H. Fournier |
| Autore | Phillips W. Pelham |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January1985 |
| Descrizione fisica | 1 online resource (97 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aerodynamic characteristics
Center of gravity Space Shuttle orbiters Wind tunnel tests Canard configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 |
| Record Nr. | UNINA-9910703860303321 |
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Phillips W. Pelham
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Space shuttle orbiter trimmed center-of-gravity extension study : summary report / / William I. Scallion and W. Pelham Phillips
| Space shuttle orbiter trimmed center-of-gravity extension study : summary report / / William I. Scallion and W. Pelham Phillips |
| Autore | Scallion William I. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , 1985 |
| Descrizione fisica | 1 online resource (50 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Center of gravity
Aerodynamic configurations Space Shuttle orbiters Wind tunnel tests Design analysis Space shuttles - Design and construction Center of mass Space vehicles - Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Space shuttle orbiter trimmed center-of-gravity extension study |
| Record Nr. | UNINA-9910709630903321 |
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Scallion William I.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities [[electronic resource] /] / Laurence D. Leavitt and James R. Burley II
| Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities [[electronic resource] /] / Laurence D. Leavitt and James R. Burley II |
| Autore | Leavitt Laurence D |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 |
| Descrizione fisica | 1 online resource (106 pages) : digital, PDF file |
| Altri autori (Persone) | BurleyJames R |
| Collana | NASA technical paper |
| Soggetto topico |
Nozzle geometry
Static tests Thrust reversal Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697180503321 |
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Leavitt Laurence D
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt
| Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt |
| Autore | Re Richard J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (110 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static tests
Thrust vector control Thrust reversal Wind tunnel tests Nozzle geometry Jet nozzles Jet planes - Thrust reversers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709716003321 |
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Re Richard J.
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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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Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/ / Laurence D. Leavitt
| Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/ / Laurence D. Leavitt |
| Autore | Leavitt Laurence D. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1985 |
| Descrizione fisica | 1 online resource (66 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Convergent
Thrust vector control Wind tunnel tests Nozzle flow Transonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709978403321 |
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Leavitt Laurence D.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1985 | ||
| 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)