Report - Aerodynamic Analysis of SMR-180-TF
All outputs of the program 'aerodynamic_analysis' were created with version 0.5.0

Data

Reference values
ParameterSymbolUnitValue
Wing half spanbm35.55
Mean aerodynamic chordMACm4.47
Reference areaSrefm2133.0
Neutral pointxm16.46
Design cruise conditions
ParameterSymbolUnitValue
Mach numberMaCr-0.78
Best L/DL/D,opt,cruise-19.17
Optimum lift coefficient at cruise (for L/D max)CL,opt,cruise-0.620
Cruise L/DL/Dcruise-18.61
Average lift coefficient at cruise (for L/Dcr)CL,cruise-0.499
Total drag at optimum lift coefficientCD,total,opt,cruise-0.03234
Induced drag at optimum lift coefficientCD,induced,opt,cruise-0.01500(46.38 %)
Viscous drag at optimum lift coefficientCD,viscous,opt,cruise-0.01595(49.32 %)
Wave drag at optimum lift coefficientCD,wave,opt,cruise-0.00139(4.30 %)
Moment coefficient at optimum lift coefficientCM,opt,cruise-0.00000
Lift coefficients
ParameterSymbolUnitValue
Max. lift coeff. landingCL,max,LD-3.135
Max. lift coeff. take-offCL,max,TO-2.681

Plots

Lift vs. Drag
Lift curve