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P

q_inf

C_L

C_D

C_M

Re

M_inf (free stream mach number)

a_inf (speed of sound)

Cl

S (wing planform area)

AR (aspect ratio)

lambda (Taper ratio)

Cdi (induced drag ratio)

Cd0

Cd

T (thrust)

P (thrust power)

C (Power Specific Fuel Consumption)

Ps-act (actual shaft power)



Pa (power available)

T (turbojet thrust)

m dot (fluid mass flow rate)



Ct (thrust fuel consumption)

Turbofan Bypass Ratio

Turboprop Pa (power available)