Aerodynamics of Flight

Dihedral Some aircraft are designed so that the outer tips of the wings are higher than the wing roots. The upward angle thus formed by the wings is called dihedral. [Figure 5-28] When a gust causes a roll, a sideslip will result. This sideslip causes the Restoring lift relative wind affecting the entire airplane to be from the direction of the slip. When the relative wind comes from the side, the wing slipping into the wind is subject to an increase in AOA and develops an increase in lift. The wing away Wing has decreased from the wind is subject to a decrease in angle of attack, and AOA, hence reduced lift develops a decrease in lift. The changes in lift effect a rolling due to sideslip. moment tending to raise the windward wing, hence dihedral Sideslip contributes to a stable roll due to sideslip. [Figure 5-29] Wing has increased AOA, hence increased lift due to sideslip. Sweepback and Wing Location Many aspects of an aircraft's configuration can affect its effective dihedral, but two major components are wing Figure 5-29. Sideslip causing different AOA on each blade. sweepback and the wing location with respect to the fuselage (such as a low wing or high wing). As a rough estimation, 10° of sweepback on a wing provides about 1° of effective dihedral, while a high wing configuration can provide about 5° of effective dihedral over a low wing configuration. A sweptback wing is one in which the leading edge slopes backward. [Figure 5-30] When a disturbance causes an aircraft with sweepback to slip or drop a wing, the low wing presents its leading edge at an angle that is more perpendicular to the relative airflow. As a result, the low wing acquires more lift, rises, and the aircraft is restored to its original flight attitude. Keel Effect and Weight Distribution Figure 5-30. Sweepback wings. A high wing aircraft always has the tendency to turn the longitudinal axis of the aircraft into the relative wind, which disturbed and one wing dips, the fuselage weight acts like a is often referred to as the keel effect. These aircraft are pendulum returning the aircraft to the horizontal level. laterally stable simply because the wings are attached in a high position on the fuselage, making the fuselage behave like Laterally stable aircraft are constructed so that the greater a keel exerting a steadying influence on the aircraft laterally portion of the keel area is above the CG. [Figure 5-31] Thus, about the longitudinal axis. When a high-winged aircraft is when the aircraft slips to one side, the combination of the Dihedral Dihedral Figure 5-28. Dihedral is the upward angle of the wings from a horizontal (front/rear view) axis of the plane as shown in the graphic depiction and the rear view of a Ryanair Boeing 737. 5-18