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87 Cards in this Set
- Front
- Back
α
|
Angle of Attack
|
|
ß
|
Sideslip Angle
|
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γ
|
Climb or Glide Angle
|
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θ
|
Pitch Attitude
|
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λ
|
Taper Ratio
|
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Λ
|
Sweep Angle
|
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μ
|
Viscosity or Coefficient of Friction
|
|
ρ
|
Air Density
|
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φ
|
Angle of Bank
|
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ω
|
Rate of Turn
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<
|
Less Than
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>
|
Greater Than
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≈
|
Approximately Equal To
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a
|
Acceleration
|
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A
|
Area
|
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AC
|
Aerodynamic Center
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AF
|
Aerodynamic Force
|
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AOA
|
Angle of Attack
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AOC
|
Angle of Climb
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AR
|
Aspect Ration
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b
|
Wing Span
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c
|
Average Chord
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CAS
|
Calibrated Airspeed
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C,D
|
Coefficient of Drag
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C,Di
|
Coefficient of Induced Drag
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C,Dp
|
Coefficient of Parasite Drag
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C,F
|
Coefficient of Aerodynamic Force
|
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CG
|
Center of Gravity
|
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C,L
|
Coefficient of Lift
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C,LMAX
|
Maximum Coefficient of Lift
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c,R
|
Root Chord
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c,T
|
Tip Chord
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d
|
Moment Arm Distance
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D
|
Drag or Adensity Altitude
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D,I
|
Induced Drag
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D,p
|
Parasite Drag
|
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D,T
|
Total Drag
|
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EAS
|
Equivalent Airspeed
|
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f
|
Equivalent Parasite Area
|
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F
|
Force
|
|
FF
|
Fuel Flow
|
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F,R
|
Rolling Friction
|
|
G
|
Acceleration of Gravity
|
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GS
|
Groundspeed
|
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IAS
|
Indicated Airspeed
|
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IAS,LDG
|
Indicated Landing Speed
|
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IAS,S
|
Indicated Stall Speed
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IAS,Sφ
|
Indicated Accelerated Stall Speed
|
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IAS,SP
|
Indicated Power-Off Stall Speed
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IAS,TO
|
Indicated Takeoff Speed
|
|
k
|
Constant
|
|
KE
|
Kinetic Energy
|
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L/D
|
Lift to Drag Ratio
|
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L
|
Lift
|
|
L,EFF
|
Effective Lift
|
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LSOS
|
Local Speed Of Sound
|
|
m
|
Mass
|
|
M
|
Mach Number
|
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M,CRIT
|
Critical Mach Number
|
|
n
|
Load Factor
|
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NP
|
Neutral Point
|
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NWLO
|
Nosewheel Liftoff Speed
|
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NWTD
|
Nosewheel Touchdown Speed
|
|
P
|
Pressure
|
|
p.e.
|
Propeller Efficiency
|
|
PE
|
Potential Energy
|
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PA
|
Pressure Altitude
|
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P,A
|
Power Available
|
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P,D
|
Power Deficit
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P,E
|
Power Excess
|
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P,S
|
Static Pressure
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P,T
|
Total Pressure
|
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q
|
Dynamic Pressure
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Q
|
Torque
|
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r
|
Radius of Turn
|
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ROC
|
Rate of CLimb
|
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RW
|
Relative Wind
|
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s
|
Distance of Displacement
|
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s,LDG
|
Landing Distance
|
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s,TO
|
Takeoff Distance
|
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S
|
Wing Surface Area
|
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SHP
|
Shaft Horsepower
|
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SRT
|
Standard Rate Turn
|
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T
|
Temperature or Thrust
|
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T,A
|
Thrust Available
|
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T,D
|
Thrust Deficit
|
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P,R
|
Power Required
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