Q1/ Choose the correct answer: 1- When all forces (lift, weight, drag, thrust) and moments about the c.g cancel out, this case called: stability equilibrium control neutrally 2- The longitudinal distance from aerodynamic center of tail to the center of gravity of aircraft: Xcg Xac It Zcg 3- The condition for an aircraft to be laterally stable is that: dCn <0 >0 dCi 20 do dCn dy dß 4- An equivalent condition for longitudinal static stability in aircraft is that: CM = 0 Әсм да OCL 5- The motion of the aircraft around its lateral axis is called: асм <0 θα <0 ac >0 yaw dcn dß <0 pitch roll

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Q1/ Choose the correct answer:
1- When all forces (lift, weight, drag, thrust) and moments about the c.g cancel out, this case called:
stability
equilibrium
control
neutrally
2- The longitudinal distance from aerodynamic center of tail to the center of gravity of aircraft:
Xcg
Xac
Zcg
3- The condition for an aircraft to be laterally stable is that:
dC₁
<0
<0
dø
dCn > 0
dß
4- An equivalent condition for longitudinal static stability in aircraft is that:
CM = 0
dcn
dy
әсм
да
OCL
5- The motion of the aircraft around its lateral axis is called:
асм <0
da
<0
ac
>0
yaw
dcn
dß
<0
pitch
roll
Transcribed Image Text:Q1/ Choose the correct answer: 1- When all forces (lift, weight, drag, thrust) and moments about the c.g cancel out, this case called: stability equilibrium control neutrally 2- The longitudinal distance from aerodynamic center of tail to the center of gravity of aircraft: Xcg Xac Zcg 3- The condition for an aircraft to be laterally stable is that: dC₁ <0 <0 dø dCn > 0 dß 4- An equivalent condition for longitudinal static stability in aircraft is that: CM = 0 dcn dy әсм да OCL 5- The motion of the aircraft around its lateral axis is called: асм <0 da <0 ac >0 yaw dcn dß <0 pitch roll
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