Info
Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / / by Millard J. Bamber
| Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / / by Millard J. Bamber |
| Autore | Bamber M. J. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (8 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Ailerons
Airplanes - Wings Rolling (Aerodynamics) Wind tunnel testing Yawing (Aerodynamics) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713646703321 |
Bamber M. J.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of blade torsion on modeling results for the small wind research turbine (SWRT) [[electronic resource] ] : preprint / / D. Corbus, National Wind Technology Center [and] A. Craig Hansen, Jeff Minnema, Windward Engineering LLC
| Effect of blade torsion on modeling results for the small wind research turbine (SWRT) [[electronic resource] ] : preprint / / D. Corbus, National Wind Technology Center [and] A. Craig Hansen, Jeff Minnema, Windward Engineering LLC |
| Autore | Corbus D |
| Pubbl/distr/stampa | Golden, CO : , : National Renewable Energy Laboratory, , [2006] |
| Descrizione fisica | 9 pages : digital, PDF files |
| Altri autori (Persone) |
HansenA. C
MinnemaJ |
| Collana | NREL/CP |
| Soggetto topico |
Wind turbines - Testing
Yawing (Aerodynamics) Aeroelasticity - Computer simulation Wind power - Research |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effect of Blade Torsion on Modeling Results for the Small Wind Research Turbine |
| Record Nr. | UNINA-9910698393903321 |
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Corbus D
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| Golden, CO : , : National Renewable Energy Laboratory, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / / J.A. Shortal
| Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / / J.A. Shortal |
| Autore | Shortal Joseph Adams <1908-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (12 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Spoilers (Airplanes)
Flaps (Airplanes) Airplanes - Control surfaces Rolling (Aerodynamics) Yawing (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716911103321 |
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Shortal Joseph Adams <1908->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effect of slots and flaps on lateral control of a low-wing monoplane as determined in flight / / by Hartley A. Soulé and J.W. Wetmore
| The effect of slots and flaps on lateral control of a low-wing monoplane as determined in flight / / by Hartley A. Soulé and J.W. Wetmore |
| Autore | Soule Hartley A (Hartley Akin), <1904-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (11 pages, 14 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Flaps (Airplanes) Slotted flaps (Airplanes) Wind tunnel testing Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715384303321 |
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Soule Hartley A (Hartley Akin), <1904-1988, >
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The estimation of the rate of change of yawing moment with sideslip / / by Frederick H. Imlay
| The estimation of the rate of change of yawing moment with sideslip / / by Frederick H. Imlay |
| Autore | Imlay Frederick H. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (12 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Testing
Yawing (Aerodynamics) Interference (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716883803321 |
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Imlay Frederick H.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight tests of retractable ailerons on a highly tapered wing / / by J.W. Wetmore
| Flight tests of retractable ailerons on a highly tapered wing / / by J.W. Wetmore |
| Autore | Wetmore Joseph W. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (9 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Flight testing
Airplanes - Wings Airplanes - Control surfaces Ailerons Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717168803321 |
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Wetmore Joseph W.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight / / by Frank G. Rokus
| Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight / / by Frank G. Rokus |
| Autore | Rokus Frank G. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (7 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Flaps (Airplanes) Split flaps (Airplanes) Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717156303321 |
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Rokus Frank G.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight / / by Th. Troller and F. Rokus
| Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight / / by Th. Troller and F. Rokus |
| Autore | Troller T. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (8 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings
Split flaps (Airplanes) Aerodynamic load - Measurement Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716990503321 |
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Troller T.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight / / by Th. Troller and F. Rokus
| Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight / / by Th. Troller and F. Rokus |
| Autore | Troller T. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (6 pages, 6 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Airplanes - Wings - Testing Flaps (Airplanes) Split flaps (Airplanes) Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717159703321 |
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Troller T.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) / / by R.H. Heald
| Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) / / by R.H. Heald |
| Autore | Heald R. H. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (12 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Ailerons
Flaps (Airplanes) Rolling (Aerodynamics) Yawing (Aerodynamics) Hinge moments (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Rolling, yawing, and hinge moments produced by rectangular ailerons |
| Record Nr. | UNINA-9910715243803321 |
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Heald R. H.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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