I have been gone a LONG time, but I have not been completely away from Civ...
^0.3=cube root
^0.5=square root
average Span(aWs)=
1 engine = 11.71
2 engines= 20.27
3 engines= 25.08
4 engines= 33.31
Jet fighter=11.81
propellor blades (X)=
2 = 8
3 = 16
4 = 20
5 = 25
Jet = 14
Armor rating (A)=
Cloth covering = +1
Aluminum = +1.5
Armor = +2
Sealing tanks = +1.5
#l = low
#m = medium
#h = high
#s = strafe
#a = attack
P= power (hp)
W= weight (kg)
Ws= Span (m)
E = engine #
V = speed (kph)
fK = forward cannons (mm)
fMG = forward MGs (mm)
RoC = rate of climb (m/sec)
R = range (km)
dMG = defensive MG (mm)
dK = defensive cannons (mm)
C = service ceiling (m)
B = bombs (kg)
Cy = cylinders
Cr = crew
#c = cost rating
Y = (P*X)/W
Z = aWs-Ws
F = ((E*P)/(100-((W+V)^0.3)))^0.5*2
Ml = ((W/Ws)^0.5+Y+F)/5
Mh = (((100*Ws)/(0.1*W))^0.5+Y+F)/5
T = (W/(E*1000)*A
MGc = 1.5*(fMG+dMG)
Kc = ((fK+dK)*1.7)/2
AtK = ((Ml+Mh)/2+fK+0.5*fMG+Z+T+RoC+R^0.3+V^0.3)^0.5
DeFl = ((Ml+fK+fMG)/2+T+dK+dMG+V^0.3+Z)^0.5
DeFm = ((Ml+Mh+fK+fMG)/2+T+dK+dMG+Z+C^0.3+V^0.3)^0.5
DeFh = ((Ml+Mh+fK+fMG)/2+T+dK+dMG+Z+C^0.5+V^0.3)^0.5
BmBs = (0.5*fK+fMG+M+Y)^0.5
BmBa = (0.5*fMG+fK+M+Y+B^0.3)^0.5
BmBm = (B/C^0.3)/10
BmBh = (B/C^0.5)/10
Cst = ((P/Cy+F+X/2+F^0.5+Cr+MGc+Kc+B^0.3+((R/2)^0.3)/2)/3)+30
^0.3=cube root
^0.5=square root
average Span(aWs)=
1 engine = 11.71
2 engines= 20.27
3 engines= 25.08
4 engines= 33.31
Jet fighter=11.81
propellor blades (X)=
2 = 8
3 = 16
4 = 20
5 = 25
Jet = 14
Armor rating (A)=
Cloth covering = +1
Aluminum = +1.5
Armor = +2
Sealing tanks = +1.5
#l = low
#m = medium
#h = high
#s = strafe
#a = attack
P= power (hp)
W= weight (kg)
Ws= Span (m)
E = engine #
V = speed (kph)
fK = forward cannons (mm)
fMG = forward MGs (mm)
RoC = rate of climb (m/sec)
R = range (km)
dMG = defensive MG (mm)
dK = defensive cannons (mm)
C = service ceiling (m)
B = bombs (kg)
Cy = cylinders
Cr = crew
#c = cost rating
Y = (P*X)/W
Z = aWs-Ws
F = ((E*P)/(100-((W+V)^0.3)))^0.5*2
Ml = ((W/Ws)^0.5+Y+F)/5
Mh = (((100*Ws)/(0.1*W))^0.5+Y+F)/5
T = (W/(E*1000)*A
MGc = 1.5*(fMG+dMG)
Kc = ((fK+dK)*1.7)/2
AtK = ((Ml+Mh)/2+fK+0.5*fMG+Z+T+RoC+R^0.3+V^0.3)^0.5
DeFl = ((Ml+fK+fMG)/2+T+dK+dMG+V^0.3+Z)^0.5
DeFm = ((Ml+Mh+fK+fMG)/2+T+dK+dMG+Z+C^0.3+V^0.3)^0.5
DeFh = ((Ml+Mh+fK+fMG)/2+T+dK+dMG+Z+C^0.5+V^0.3)^0.5
BmBs = (0.5*fK+fMG+M+Y)^0.5
BmBa = (0.5*fMG+fK+M+Y+B^0.3)^0.5
BmBm = (B/C^0.3)/10
BmBh = (B/C^0.5)/10
Cst = ((P/Cy+F+X/2+F^0.5+Cr+MGc+Kc+B^0.3+((R/2)^0.3)/2)/3)+30