Aero 1-6
Aerodynamic 081
Aerodynamic 081
Kartei Details
| Karten | 34 |
|---|---|
| Sprache | English |
| Kategorie | Physik |
| Stufe | Andere |
| Erstellt / Aktualisiert | 07.12.2016 / 08.12.2016 |
| Lizenzierung | Keine Angabe (-) |
| Weblink |
https://card2brain.ch/box/aero_16
|
| Einbinden |
<iframe src="https://card2brain.ch/box/aero_16/embed" width="780" height="150" scrolling="no" frameborder="0"></iframe>
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When flaps are deployed at constant AoA, lift coefficientw will...
increase!
Flap selcetion at constant IAS in S&L flight will increase the...
max. lift coefficient (CLmax) and the drag.
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.
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.
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.
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
The rotation about the NORMAL axis is...
yawing!
The elevtaor deflection required for a given manoeuvre will be:
smaller at high IAS when compared to low IAS.
