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for supersonic(passive) was designedswept wing
One is trimming rear spareto setwing " sweep
using a soldering ironto setthe wing sweep
very happysettingthe wing sweep
The boundary layer outflowalso resultingfrom 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
the line of the 25 % chord line(passive) is set byThe sweep of a wing
Football CoachcreatedWing Draw Sweep
less dragcreateless drag
pitching momentwill contributepitching moment
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 airflow to be deflected outwardscausesthe airflow to be deflected outwards
to AUTOsetto AUTO
a yaw - induced rolling momentcausesa yaw - induced rolling moment
backcausesback
negative rollalso causesnegative roll
to apparent dihedral effectalso contributesto apparent dihedral effect
structural damage the aircraft ormight ... causestructural damage the aircraft or
a flattening of the lift curve slope for two reasonscausesa flattening of the lift curve slope for two reasons
Land - based fire controlsettingLand - based fire control
to effective dihedralcontributesto effective dihedral
incidence(passive) being influenced byincidence
the static moment(passive) caused bythe static moment