The layers are cut chunky and choppy, leaving the layer at the uppermost part of the head just a bit longer so it can be worn several ways. The nape is cut very close, and top and sides are layered but are long enough to allow curls to A bold rose pink adds a new flavor to an undercut pixie, and the short sides separated from the longer, disconnected top by a shaved-in part line. At approximately thirty percent (30%) outboard of its inboard end, the conical slat 28A is supported and actuated by a linkage system. As is conventional, the leading edge slat systems are structurally supported forward of the wing front spar 21.A wing trailing edge high-lift system is also provided comprising double-slotted flaps 30 in the "Yehudi" section 11 (inboard flaps) and double-slotted flaps 31 outboard thereof (outboard flaps). The combination of claim 16, wherein a spanwise varying aerodynamic slot opening is formed during forward extension of said wing tip member leading edge device relative to the fixed portion of said wing tip member, said slot opening decreasing in a spanwise outboard direction.19. Adding a wing tip extension member will increase cost and weight if the tip extension must have a leading edge device, such as a slat.

This aft load on the tip extension produces a moment that tends to twist the wing leading edge down at higher maneuver and gust loads, thus reducing incidence angle and lift coefficient. More recent works have investigated straight pin fins with complex geometries including elliptical [1], [2], [5], [10]–[15], square [5], [16], [17], triangular [5], [6], airfoil derived [5], [13], and teardrop cross-sections [5], [11], [13], [18]. The nape is cut short with a point at the back left corner, balancing out the first point to complete the look.

The absence of a leading edge device on a wing tip extension member could produce undesirable effects, such as premature stall, on the wing tip extension member. The center of pressure of the tip extension 12 is aft of the neutral axis for torsion of the main wing 10. Any span increase causes increased bending moments on the existing wing and requires an increase in the structural strength of the existing wing box. In its forward/outboard part the pod houses the red/green position lights and the anticollision strobes for the forward/side quadrant.

is buzzed very close in this pixie, revealing a line or design (again of your choosing) for added edginess. The increase in aerodynamic airloads causes high wing bending moments requiring significant structural redesign and strengthening of the basic wing box from the root section of the main wing to the outboard section of the wing tip extension member.A third approach for theoretically increasing the aspect ratio of a sweptback tapered main wing is the use of end plates or wing tip fins to significantly reduce wing tip vortices and the drag induced thereby. The apparatus of claim 3, wherein each wing tip member has a center of pressure further aft of the neutral axis for torsion of said main wing, whereby when said aircraft experiences a gust at high speed cruise conditions above Mach 0.7, said wing tip member produces a moment that aeroelastically twists said main wing to unload and decrease main wing bending moments.6. Ideal for natural waves, this cut can be styled easily with a quick blow dry and side part, lifting the roots, or a slightly wavy texture can be added with an iron as well.

3, or about six percent (6%) of semispan of the main wing 10.

11 is a chordwise cross-sectional view taken in the direction indicated by line 11--11 of FIG. With the length left on top, the cut can be spiked, worn forward, or side-parted for several different looks.

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