Karten 34 Karten
Lernende 1 Lernende
Sprache English
Stufe Andere
Erstellt / Aktualisiert 07.12.2016 / 08.12.2016
Lizenzierung Keine Angabe     (-)
3 Exakte Antworten 31 Text Antworten 0 Multiple Choice Antworten
Fenster schliessen

When flaps are deployed at constant AoA, lift coefficientw will...

Fenster schliessen

Flap selcetion at constant IAS in S&L flight will increase the...

max. lift coefficient (CLmax) and the drag.
Fenster schliessen

Difference between the effects of flap and slat asymettry is that...

flaps asymmetry causes a large rolling moment at any speed,

whereas slat asymmetry causes a large difference in CLmax.

Fenster schliessen

The use of slat in leading edge of the wing enables the aeroplane to fly at a slower speed because...

it delays the stall to a higher angle of attack.

Fenster schliessen

When spoliers are extended the part of the wing which they are mounted...

experiences a reduction in lift, which generates the desired rolling moment, additionally

there is a local increase in drag, which suppresses adverse yaw.

Fenster schliessen

What happens with drag and lift -> wing spoiler extension in S&L flight, the speed and load factor are constant...

drag increases,

lift remains unaffected

Fenster schliessen

The rotation about the NORMAL axis is...

Fenster schliessen

The elevtaor deflection required for a given manoeuvre will be:

smaller at high IAS when compared to low IAS.