Chapter 16: Lift Augmentation Flashcards
TE Flap Types
Plain Flap
Split Flap
Slot
Fowler
Plain TE Flap
Clmax, AoAs, CP
+ Clmax (camber)
- AoAs (rounder wing)
CP aft (homogeneous L distribution)
Split TE Flap
Clmax, AoAs, Drag
Why is 3rd element good (2)
\+ Clmax (camber) - AoAs (less AoAs loss than plain because wing top not deformed High drag penalty -> high thrust = Vs increase and = reactive engines
TE Slot
AoAs
TE Fowler
Clmax, Surface, AoAs
Slot: \+ AoAs (reenergises flow) Fowler: \+ Clmax (camber) \+ Surface \+ AoAs
LE Flap Types (4)
Plain LE Flap
Krueger LE Flap
Slot
Slat
Plain LE Flap
AoAs, Clmax
+ AoAs (increases LE radius -> less energy loss)
+ Clmax (camber)
Slot
AoAs, Clmax
+ AoAs (reenergises flow)
-> + Clmax
Krueger LE Flap
What is it, where to put for sweptback wings
Plain LE Flap with hook (if stag. point below Krueger flap -> stall)
Sweptback wing = root
LE Flap or Slat
LE Slot + LE Plain Flap
Plain, Splitted, Slotted, Fowler
In Order of Drag
In Order of Clmax
Drag (+ to -) : split, plain, slotted, fowler
Clmax (+ to -) : fowler, slotted, split, plain
Flaps at root and vortices
Flaps @ root = less L at tip = less tip vortices
Flaps and Pitch (2)
Cp aft -> pitch down
root downwash -> more elevator downforce -> pitch up (tailplane effect)
Lift Renergizing Devices (3)
Vortex generators (turbulent air ailerons)
Strakes (sharp symmetric airfoils on AC)
Chines (on engine)
TO Flap
What do when retract flaps
Effect of Flap on Cl Cd
Flap retract = pitch up for L constant
50% flap - high increase Cl, small increase Cd
100% flap - low increase Cl, high increase Cd
Flap Asymmetry
Which is worse, LE Flaps or TE Flaps? How to prevent
Flap worse -> for same AoA, higher Cl increase
Longer landing
Flap asymmetry sensor