本帖最后由 LJQC 于 2011-11-18 14:48 编辑
From 1F-16CJ-1~~划一下要点
CROSSWIND LANDING
The recommended technique for landing in a crosswind is to use a wing level crab through touchdown. At touchdown, the ARI switches out. Undesirable yaw transients may occur if roll control is being applied at this time.(wing level crab就是在接地时机身保持水平,航迹保持不变的一种着陆方式,有别于De-Crab和Sideslip。ARI详见http://bbs.3gofly.com/bbs/thread-203341-1-1.html)
After touchdown, perform twopoint aerodynamic braking(这个在13AOA时的效果是最好的)using the rudder to maintain aircraft track down the runway and flaperon to prevent wing rise. In crosswinds, the aircraft may drift downwind due to side loads imposed by the crosswinds or travel upwind due to insufficient directional control inputs/availability.
As the airspeed decreases, increasing amounts of rudder are required to maintain track. Maintain twopoint aerodynamic braking until approximately 100 knots or until roll or directional control becomes a problem. As the pitch attitude decreases, the nose tends to align itself with the ground track.
Aft stick and fully opened speedbrakes reduce stopping distance. Apply brakes after nosewheel is on the runway; however, if stopping distance is a factor, refer to SHORT FIELD LANDING, this section. With all LG on the runway, maintain directional control with rudder, differential braking, and NWS if required.(Differential Braking可以使左右脚刹车力度不同,以达到小幅度修正方向的效果。按住SPD BRK Switch可以使减速板从43度开到60度)
During landing rollout, the main concerns are wing rise (roll control), weathervaning (directional control), and downwind drift. Wing rise is controlled by flaperon into the crosswind. Excessive flaperon deflection degrades directional control. Use rudder and differential braking to control ground track, especially on wet or icy runways. Engage NWS if required to maintain directional control and to prevent departure from the runway. Excessive differential braking may result in a hot brake condition. High rudder pedal force may result in a yaw transient when NWS is engaged. NLG strut compression is required to engage NWS but sustained forward stick may result in full horizontal tail deflection which decreases weight on the MLG and thus reduces wheel braking effectiveness. NWS engagement may be required with the drag chute deployed to control increased weathervaning tendencies. However, the nose up pull of the drag chute may prevent early NWS engagement. |