weightsintemp.dat

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 ==== Weights Analysis Input File ====

rho = 0.0021
vel = velocity
Swing = wingarea
Nzult = 5.7
AR = aspectratio
Length = fuselength
Diameter = fusediameter
Wfuel = weightfuel
Wen = weightengine
Nen = numberofengines
Npass = numberofpassengers
Wpay = weightofpayload