The boundary layer outflowalso resultingfrom wing sweep
instructionsto setcorrect wing sweep
to increase Mcrit(passive) is designedWing sweep
that the flaps do not fully retract back into the wing after the G is releasedthus preventingany wing sweep
the spanwise pressure gradientresultingfrom the wing sweep
Football CoachcreatedWing Draw Sweep
less dragcreateless drag
pitching momentwill contributepitching moment
the airflow to be deflected outwardscausesthe airflow to be deflected outwards
the development of the shock wave at the leading edge ( Figure 1.7preventsthe development of the shock wave at the leading edge ( Figure 1.7
the illusion of anhedralcan ... createthe illusion of anhedral
alsocontributedalso
to AUTOsetto AUTO
a yaw - induced rolling momentcausesa yaw - induced rolling moment
backcausesback
negative rollalso causesnegative roll
in “ a more integrated design that significantly improved vehicle performanceresultingin “ a more integrated design that significantly improved vehicle performance
structural damage the aircraft ormight ... causestructural damage the aircraft or
to apparent dihedral effectalso contributesto apparent dihedral effect
Land - based fire controlsettingLand - based fire control
incidence(passive) being influenced byincidence
a flattening of the lift curve slope for two reasonscausesa flattening of the lift curve slope for two reasons
to effective dihedralcontributesto effective dihedral
the static moment(passive) caused bythe static moment