Flaps y slats

Airbus A320

Nociones generales

Airbus A380

Aproximación y aterrizaje con flaps Fowler de 1 ranura

Boeing 747

Despegue con flaps Fowler de 2 ranuras

Boeing 747

Aproximación y aterrizaje con flaps Krueger de curvatura variable 

Boeing 747

Aterrizaje con flaps Fowler de 3 ranuras

Boeing 767

Aterrizaje con flap Fowler externo de 1 ranura

Boeing 737

Aproximación y aterrizaje con flaps Fowler de 2 ranuras

Boeing 747

Flap Krueger

Boeing 737

Flap Fowler de 3 ranuras

Boeing 727

Flap Fowler de 3 ranuras

Boeing 747

Vista de los flaps Krueger en el borde de ataque y de los

flaps Fowler de 3 ranuras durante la aproximación y el aterrizaje

 

Documentación técnica:

 

A review of current leading edge device technology and of options for innovation based on flow control
Autores: Helen Heap y Bill Crowther
A review of current leading edge device [...]
Documento Adobe Acrobat [215.8 KB]
Aerodynamic characteristics of a wing with Fowler flaps including flap loads, downwash, and calculated effect on take-off
Autor: Robert C. Platt
Fuente: NACA
Aerodynamic characteristics of a wing wi[...]
Documento Adobe Acrobat [1.1 MB]
Aerodynamics loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section
Autores: John A. Kelly y George B. McCullough
Fuente: NACA
Aerodynamics loads on a leading-edge fla[...]
Documento Adobe Acrobat [1.0 MB]
Airfoils with dynamic transonic flow control
Autores: M. Trenker, W. Geissler y H. Sobieczky
Airfoils with dynamic transonic flow con[...]
Documento Adobe Acrobat [192.1 KB]
Aspectos del control de flujo con un flap Gurney rotante sobre un perfil NACA 4412
Autores: Mauricio E. Camocardi, Juan S, Delnero, Julio Marañón Di Leo, Jorge L. Colman Lerner, Federico Muñoz y Mariano O. García Sainz
Aspectos del control de flujo con un fla[...]
Documento Adobe Acrobat [625.7 KB]
Calculated effect of various tipes of flap on take-off over obstacles
Autor: J. W. Wetmore
Fuente: NACA
Calculated effect of various tipes of fl[...]
Documento Adobe Acrobat [909.7 KB]
Collection of test data for lateral control with full-span flaps
Autores: Jack Fischel y Margaret F. Ivery
Fuente: NACA
Collection of test data for lateral cont[...]
Documento Adobe Acrobat [10.0 MB]
Comportamiento aerodinámico de cuerpos fuselados y perfiles alares
Autores: Arturo Velásquez S. y Claudio Velásquez S.
Comportamiento aerodinámico de cuerpos f[...]
Documento Adobe Acrobat [1.0 MB]
Control de flujo sobre la estela cercana de perfiles aerodinámicos mediante la implementación de mini-flaps Gurney
Autor: Mauricio E. Camocardi
Control de flujo sobre la estela cercana[...]
Documento Adobe Acrobat [2.5 MB]
Effects of a leading-edge slat and a trailing-edge split flap on the aerodynamic characteristics of a wing-fuselage combination having a nearly triangular wing of aspect ra
Autor: Fred A. Demele
Fuente: NACA
Effects of a leading-edge slat and a tra[...]
Documento Adobe Acrobat [3.5 MB]
Effect of slats and flaps on a finite wing
Autor: David F. Rogers
Effect of slats and flaps on a finite wi[...]
Documento Adobe Acrobat [102.0 KB]
Experiments with slotted wings
Autor: L. Lachmann
Fuente: NACA
Experiments with slotted wings.pdf
Documento Adobe Acrobat [1.3 MB]
Force and pressure-distribution measurements on a rectangular wing with a slotted droop nose and with either plain and split flaps in combination or a slotted flap
Autor: H. G. Lemme
Fuente: NACA
NACA 1108 Force and Pressure Distributio[...]
Documento Adobe Acrobat [830.2 KB]
High-lift aerodynamics
Autor: W.H. Mason
High-lift aerodynamics.pdf
Documento Adobe Acrobat [669.3 KB]
Investigation at low speed of the longitudinal stability characteristics of a 60º swept-back tapered low-drag wing
Autores: John G. Lowry y Leslie E. Schneider
Fuente: NACA
Investigation at low speed of the longit[...]
Documento Adobe Acrobat [1.5 MB]
Investigation of a slat in several different positions on an NACA 64A010 airfoil for a wide range of subsonic mach numbers
Autores: John A. Axelson y George L. Stevens
Fuente: NACA
Investigation of a slat in several diffe[...]
Documento Adobe Acrobat [1.2 MB]
Lift increase by blowing out air, tests on airfoil of 12 percent thickness, using various types of flap
Autor: W. Schwier
Fuente: NACA
Lift increase by blowing out air, tests [...]
Documento Adobe Acrobat [1.2 MB]
Low-speed aerodynamic characteristics of a large-scale 45º swept-back wing with partial-span slats, double-slotted flaps, and ailerons
Autor: Harry A. James
Fuente: NACA
Low-speed aerodynamic characteristics of[...]
Documento Adobe Acrobat [2.9 MB]
Low-speed wind-tunnel tests of Fowler flaps, slats and nose flaps on a model of a jet aircraft with a 40 deg swept-back wing
Autor: A. Spence, B.Sc.
Low-speed wind-tunnel tests of Fowler fl[...]
Documento Adobe Acrobat [919.5 KB]
Mecánica de vuelo
Fuente: AENA
Mecánica de vuelo.pdf
Documento Adobe Acrobat [980.9 KB]
Parametric airfoils and wings
Autor: Helmut Sobieczky
Parametric airfoils and wings.pdf
Documento Adobe Acrobat [260.4 KB]
Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap
Autores: Carl J. Wenzinger y James B. Delano
Fuente: NACA
Pressure distribution over an NACA 23012[...]
Documento Adobe Acrobat [1.2 MB]
Pressure distribution over airfoils with Fowler flaps
Autores: Carl J. Wenzinger y Walter B. Anderson
Fuente: NACA
Pressure distribution over airfoils with[...]
Documento Adobe Acrobat [821.1 KB]
Pressure distribution over an NACA 23012 airfoil with an NACA 23012 external-airfoil flap
Autor: Carl J. Wenzinger
Fuente: NACA
Pressure distribution over an NACA 23012[...]
Documento Adobe Acrobat [678.2 KB]
Résumé of air-load data on slats and flaps
Autores: Carl J. Wezinger y Francis M. Rogallo
Fuente: NACA
Résumé of air-load data on slats and fla[...]
Documento Adobe Acrobat [1.1 MB]
Review of aircraft aerodynamics
Review of aircraft aerodynamics.pdf
Documento Adobe Acrobat [219.6 KB]
Systematic wind-tunnel measurements on a laminar wing with nose flap
Autor: W. Krueger
Fuente: NACA
Systematic wind-tunnel measurements on a[...]
Documento Adobe Acrobat [704.1 KB]
The characteristics of a Clark Y wing model equipped with several forms of low-drag fixed slots
Autores: Fred E. Weick y Carl J. Wenzinger
Fuente: NACA
The characteristics of a Clark Y wing mo[...]
Documento Adobe Acrobat [547.8 KB]
The effect of a flap and ailerons on the NACA M-6 airfoil section
Autores: George J. Higgins y Eastman N. Jacobs
Fuente: Langley Memorial Aeronautical Laboratory
The effect of a flap and ailerons on the[...]
Documento Adobe Acrobat [1'020.9 KB]
Theory of the slotted wing
Autor: A. Betz
Fuente: NACA
Theory of the slotted wing.pdf
Documento Adobe Acrobat [831.2 KB]
Two-dimensional wind-tunnel investigation of the NACA 64-012 airfoil equipped with two types of leading-edge flap
Autor: Felicien F. Fullmer, Jr.
Fuente: NACA
Two-dimensional wind-tunnel investigatio[...]
Documento Adobe Acrobat [864.8 KB]
Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane wite blowing flaps and leading-edge slats
Autores: Harry A. James y Ralph L. Maki
Fuente: NACA
Wind-tunnel tests of the static longitud[...]
Documento Adobe Acrobat [1.2 MB]
Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot
Autores: Fred E. Weick y Robert C. Platt
Fuente: NACA
Wind-tunnel tests on model wing with Fow[...]
Documento Adobe Acrobat [478.1 KB]
Wind-tunnel tests of the Fowler variable-area wing
Autores: Fred E. Weick y Robert C. Platt
Fuente: NACA
Wind-tunnel tests of the Fowler variable[...]
Documento Adobe Acrobat [406.9 KB]