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Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section / / by Hamilton A. Smith and Raymond F. Schaefer
| Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section / / by Hamilton A. Smith and Raymond F. Schaefer |
| Autore | Smith Hamilton A. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Aerodynamics Lift (Aerodynamics) Drag (Aerodynamics) Pitching (Aerodynamics) Reynolds number |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section |
| Record Nr. | UNINA-9910713757103321 |
Smith Hamilton A.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10⁶ to 9.0 x 10⁶ / / by Laurence K. Loftin, Jr. and Hamilton A. Smith
| Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10⁶ to 9.0 x 10⁶ / / by Laurence K. Loftin, Jr. and Hamilton A. Smith |
| Autore | Loftin Laurence K. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949 |
| Descrizione fisica | 1 online resource (75 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Aerodynamics Reynolds number Aerodynamic characteristics Airfoil profiles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of fifteen National Advisory Committee for Aeronautics airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6) |
| Record Nr. | UNINA-9910713762603321 |
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Loftin Laurence K.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949 | ||
| 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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Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham
| Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham |
| Autore | Noonan Kevin W. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980 |
| Descrizione fisica | 1 online resource (82 pages) : chiefly illustrations |
| Collana |
NASA technical paper
AVRADCOM technical report |
| Soggetto topico |
Aerodynamic characteristics
Airfoils Helicopters Reynolds number Wind tunnel tests Aerofoils - Testing Helicopters - Aerodynamics Rotors (Helicopters) - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707473303321 |
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Noonan Kevin W.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic characterization of a thin, high-performance airfoil for use in ground fluids testing / / Andy P. Broeren, Sam Lee, Catherine Clark
| Aerodynamic characterization of a thin, high-performance airfoil for use in ground fluids testing / / Andy P. Broeren, Sam Lee, Catherine Clark |
| Autore | Broeren Andy P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013 |
| Descrizione fisica | 1 online resource (24 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic characteristics
Ice formation Leading edges Reynolds number Thin airfoils Deicers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702742303321 |
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Broeren Andy P.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic effects of high turbulence intensity on a variable-speed power-turbine blade with large incidence and Reynolds number variations / / Ashlie B. Flegel, Paul W. Giel, Gerard E. Welch
| Aerodynamic effects of high turbulence intensity on a variable-speed power-turbine blade with large incidence and Reynolds number variations / / Ashlie B. Flegel, Paul W. Giel, Gerard E. Welch |
| Autore | Flegel Ashlie B. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2014 |
| Descrizione fisica | 1 online resource (21 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic turbines
Aerodynamic characteristics Turbulence effects Turbine blades Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703640003321 |
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Flegel Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2014 | ||
| 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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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch
| Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch |
| Autore | McVetta Ashlie B. |
| Edizione | [Revised copy.] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 |
| Descrizione fisica | 1 online resource (23 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic turbines
Turbine blades Aerodynamic heat transfer Computational fluid dynamics Reynolds number Pressure distribution Inlet flow Angles (geometry) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702656103321 |
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McVetta Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade / / Ashlie B. Flegel
| Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade / / Ashlie B. Flegel |
| Autore | Flegel Ashlie B. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014 |
| Descrizione fisica | 1 online resource (iv, 36 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Reynolds number
Turbine blades Rotor blades (turbomachinery) Tilt rotor aircraft Three dimensional flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703642403321 |
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Flegel Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers / / R.J. Boyle [and four others]
| Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers / / R.J. Boyle [and four others] |
| Autore | Boyle Robert J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1998 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamics
Turbines Stators Transition points Reynolds number Flow measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705858403321 |
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Boyle Robert J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Reynolds number
(64)
- Mach number (18)
- Wind tunnel tests (10)
- Aerodynamics (9)
- Aerodynamic characteristics (8)