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Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel [[electronic resource] /] / Richard P. Woodward and Christopher E. Hughes
| Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel [[electronic resource] /] / Richard P. Woodward and Christopher E. Hughes |
| Autore | Woodward Richard P |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (76 pages) : illustrations (some color) |
| Altri autori (Persone) | HughesChristopher E |
| Collana | NASA/TM |
| Soggetto topico |
Acoustic properties
Noise intensity Aerodynamic characteristics Mach number Angle of attack Air flow |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Acoustic performance of the General Electric Aircraft Engines Universal Propulsion Simulator research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel |
| Record Nr. | UNINA-9910702122303321 |
Woodward Richard 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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Acoustically excited heated jets / / J. Lepicovsky [and four others]
| Acoustically excited heated jets / / J. Lepicovsky [and four others] |
| Autore | Lepicovsky Jan |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information, , June 1988 |
| Descrizione fisica | 1 online resource (3 volumes) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Flow visualization
Acoustic excitation Jet flow Mach number Fluid mechanics Jets - Fluid dynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | I. Internal excitation -- II. In search of a better understanding -- III. Mean flow data. |
| Record Nr. | UNINA-9910709874003321 |
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Lepicovsky Jan
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information, , June 1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ / / by Laurence K. Loftin, Jr
| Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ / / by Laurence K. Loftin, Jr |
| Autore | Loftin Laurence K. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Aerodynamics Mach number Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of the National Advisory Committee for Aeronautics 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6) |
| Record Nr. | UNINA-9910713887303321 |
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Loftin Laurence K.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 / / by Paige B. Burbank and Robert W. Byrne
| The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 / / by Paige B. Burbank and Robert W. Byrne |
| Autore | Burbank Paige B. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 |
| Descrizione fisica | 1 online resource (37 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Nozzles - Fluid dynamics
Mach number Supersonic nozzles - Design and construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713892903321 |
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Burbank Paige B.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic effects of simulated ice accretion on a generic transport model [[electronic resource] /] / Andy P. Broeren ... [and others]
| Aerodynamic effects of simulated ice accretion on a generic transport model [[electronic resource] /] / Andy P. Broeren ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (17 pages) : illustrations (some color) |
| Altri autori (Persone) | BroerenAndy P |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic characteristics
Aerodynamic drag Ice formation Flow visualization Horizontal tail surfaces Mach number Reynolds number Scale models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701915903321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / / George T. Carson, Jr., and Milton Lamb
| Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / / George T. Carson, Jr., and Milton Lamb |
| Autore | Carson George T. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , June 1988 |
| Descrizione fisica | 1 online resource (171 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Nozzle geometry
Mach number Hypersonic nozzles Ramjet engines Nozzle efficiency Jet nozzles - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709877103321 |
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Carson George T.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , June 1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Airfoil section characteristics at high angles of attack / / by Laurence K. Loftin, Jr
| Airfoil section characteristics at high angles of attack / / by Laurence K. Loftin, Jr |
| Autore | Loftin Laurence K. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Angle of attack (Aerodynamics) Lift (Aerodynamics) Mach number Reynolds number Surface roughness |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713887603321 |
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Loftin Laurence K.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima
| Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (36 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Supersonic wind tunnels Acoustic resonance Frequency response High frequencies Mach number Inlet pressure Supersonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702114103321 |
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Chima Rodrick V
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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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Automated boundary conditions for wind tunnel simulations / / Jan-Renee Carlson
| Automated boundary conditions for wind tunnel simulations / / Jan-Renee Carlson |
| Autore | Carlson Jan-Renee |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2018 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations (mostly color) |
| Collana | NASA/TM |
| Soggetto topico |
Boundary conditions
Computational fluid dynamics Wind tunnels Simulation Mach number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706987803321 |
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Carlson Jan-Renee
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Calibration of 30° included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.51 / / Walter A. Vahl and Robert L. Weirich
| Calibration of 30° included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.51 / / Walter A. Vahl and Robert L. Weirich |
| Autore | Vahl Walter A. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 |
| Descrizione fisica | 1 online resource (39 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Base flow
Supersonic transports Base flow (Aerodynamics) Cone - Aerodynamics Mach number Supersonic transport planes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715970103321 |
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Vahl Walter A.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Mach number
(71)
- Reynolds number (18)
- Angle of attack (9)
- Wind tunnel tests (9)
- Computational fluid dynamics (8)