1
Q
Mean Aerodynamic Chord
A
An imaginary rectangular wing with the same pitching characteristics of the swept back wing.
- Leading Edge (LeMAC)
- Trailing Edge (TeMAC)
LeMAC = 0% MAC TeMAC = 100% MAC
MAC remains constant
2
Q
CofG as a %MAC
A
CofG%MAC = (CG Arm - LeMAC / MAC) x 100
%
%MAC = (LeMAC to CG/MAC) x 100
Mass And Balance
flashcards
Decks in class (12)
# Cards
-
Ch 1 - Units And Conversions5
-
Ch 2 - Aircraft Mass Definitions25
-
Ch 3 - Allowed Take-Off Mass10
-
Ch 4 - Maximum Traffic And Fuel Load5
-
Ch 5 - Cargo Loading And Limitations12
-
Ch 7 - Datum, Moments And Determining CofG5
-
Ch 8 - MAC And CofG Position2
-
Ch 6 - The Effect Of Mass An Its Distribution20
-
Ch 8 - MAC And CG Position4
-
Ch 9 - Adjusting CG Position5
-
Ch 10 - Methods For Weighing AC4
-
Ch 11 - Weighing Pax, Crew And Baggage3
