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Active spanwise lift control : a distributed parameter approach / / Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), São José dos Campos, São Paulo, Brazil, James E. Hubbard, Jr., TEES Eminent Professor, Hagler Institute Fellow, Department of Mechanical Engineering, Texas A&M University, College Station, Texas, USA, Glenn L. Martin Professor Emeritus, University of Maryland, College Park
| Active spanwise lift control : a distributed parameter approach / / Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), São José dos Campos, São Paulo, Brazil, James E. Hubbard, Jr., TEES Eminent Professor, Hagler Institute Fellow, Department of Mechanical Engineering, Texas A&M University, College Station, Texas, USA, Glenn L. Martin Professor Emeritus, University of Maryland, College Park |
| Autore | Dias Joaquim Neto |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2020] |
| Descrizione fisica | 1 online resource (205 pages) |
| Disciplina | 629.13233 |
| Soggetto topico |
Gust loads
Lift (Aerodynamics) Trailing edge flaps Airplanes - Wings |
| ISBN |
1-62410-630-7
1-5231-4093-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910795900903321 |
Dias Joaquim Neto
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| Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2020] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Active spanwise lift control : a distributed parameter approach / / Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), São José dos Campos, São Paulo, Brazil, James E. Hubbard, Jr., TEES Eminent Professor, Hagler Institute Fellow, Department of Mechanical Engineering, Texas A&M University, College Station, Texas, USA, Glenn L. Martin Professor Emeritus, University of Maryland, College Park
| Active spanwise lift control : a distributed parameter approach / / Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), São José dos Campos, São Paulo, Brazil, James E. Hubbard, Jr., TEES Eminent Professor, Hagler Institute Fellow, Department of Mechanical Engineering, Texas A&M University, College Station, Texas, USA, Glenn L. Martin Professor Emeritus, University of Maryland, College Park |
| Autore | Dias Joaquim Neto |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2020] |
| Descrizione fisica | 1 online resource (205 pages) |
| Disciplina | 629.13233 |
| Soggetto topico |
Gust loads
Lift (Aerodynamics) Trailing edge flaps Airplanes - Wings |
| ISBN |
1-62410-630-7
1-5231-4093-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910806984003321 |
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Dias Joaquim Neto
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| Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2020] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris
| The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 |
| Descrizione fisica | 1 online resource (7 pages, 11 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Wind tunnel testing
Split flaps (Airplanes) Airplanes - Models - Wings Trailing edge flaps |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713650303321 |
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Weick Fred E.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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AFC-enabled simplified high-lift system integration study / / Peter M. Hartwich [and seven others]
| AFC-enabled simplified high-lift system integration study / / Peter M. Hartwich [and seven others] |
| Autore | Hartwich Peter M. |
| Pubbl/distr/stampa | Hampton, Virginia. : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 |
| Descrizione fisica | 1 online resource (v, 31 pages) : color illustrations, maps |
| Collana | NASA/CR |
| Soggetto topico |
Lift devices
Leading edge slats Aerodynamic characteristics Navier-Stokes equation Trailing edge flaps Drooped airfoils |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Active Flow Control enabled simplified high lift system integration study |
| Record Nr. | UNINA-9910702730803321 |
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Hartwich Peter M.
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| Hampton, Virginia. : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The calculated effect of trailing-edge flaps on the take-off of flying boats / / by J.B. Parkinson and J.W. Bell
| The calculated effect of trailing-edge flaps on the take-off of flying boats / / by J.B. Parkinson and J.W. Bell |
| Autore | Parkinson John B. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (15 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Seaplanes
Airplanes - Takeoff Trailing edge flaps Trailing edges (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715921903321 |
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Parkinson John B.
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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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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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Wind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots / / by William E. Gauvain
| Wind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots / / by William E. Gauvain |
| Autore | Gauvain William E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 |
| Descrizione fisica | 1 online resource (6 pages, 9 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings
Leading edges (Aerodynamics) Trailing edge flaps Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716799203321 |
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Gauvain William E.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot / / by Fred E. Weick and Robert C. Platt
| Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot / / by Fred E. Weick and Robert C. Platt |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (10 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Airplanes - Control surfaces Flaps (Airplanes) Leading edge flaps Trailing edge flaps Slotted flaps (Airplanes) Fowler flaps Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715227303321 |
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Weick Fred E.
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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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