print("Nominal mission fuel = ",
"%.1f" % (aircraft.nominal_mission.block_fuel), " kg")
print("")
print("Take off field length required = ",
"%.1f" % aircraft.low_speed.req_tofl, " m")
print("Take off field length effective = ",
"%.1f" % aircraft.low_speed.eff_tofl, " m")
print("")
print("Approach speed required = ",
"%.1f" % unit.kt_mps(aircraft.low_speed.req_app_speed), " kt")
print("Approach speed effective = ",
"%.1f" % unit.kt_mps(aircraft.low_speed.eff_app_speed), " kt")
print("")
print("Vertical speed required = ",
"%.1f" % unit.ftpmin_mps(aircraft.high_speed.req_vz_climb), " ft/min")
print("Vertical speed effective = ",
"%.1f" % unit.ftpmin_mps(aircraft.high_speed.eff_vz_climb), " ft/min")
print("")
print("Time to climb required = ",
"%.1f" % unit.min_s(aircraft.high_speed.req_ttc), " min")
print("Time to climb effective = ",
"%.1f" % unit.min_s(aircraft.high_speed.eff_ttc), " min")
print("")
print("Cash Operating Cost = ",
"%.1f" % aircraft.economics.cash_operating_cost, " $/trip")
print("Carbon dioxid emission = ", "%.1f" % (aircraft.cost_mission.block_CO2),
" kg/trip")
print("Fuel efficiency metric = ",
"%.4f" % (aircraft.environmental_impact.CO2_metric * 1e7),
perform.handling_qualities_analysis(aircraft)
print("-------------------------------------------")
print("Handling qualities analysis : done")
print("")
print("Rayon d'action demandé = ","%.0f"%unit.NM_m(aircraft.design_driver.design_range)," NM")
print(" . . . . . . . effectif = ","%.0f"%unit.NM_m(aircraft.nominal_mission.range)," NM")
print("")
print("Longueur de piste au décollage demandée = "+"%.0f"%aircraft.low_speed.req_tofl+" m")
print(" . . . . . . . . . . . . . . . effective = "+"%.0f"%aircraft.low_speed.eff_tofl+" m")
print("")
print("Vitesse d'approche demandée = "+"%.1f"%unit.kt_mps(aircraft.low_speed.req_app_speed)+" kt")
print(" . . . . . . . . . effective = "+"%.1f"%unit.kt_mps(aircraft.low_speed.eff_app_speed)+" kt")
print("")
print("Vitesse de monté demandé = "+"%.1f"%unit.ftpmin_mps(aircraft.high_speed.req_vz_climb)+" ft/min")
print(" . . . . . . . . effective = "+"%.1f"%unit.ftpmin_mps(aircraft.high_speed.eff_vz_climb)+" ft/min")
print("")
print("Temps de monté demandé = "+"%.1f"%unit.min_s(aircraft.high_speed.req_ttc)+" min")
print(" . . . . . . . effectif = "+"%.1f"%unit.min_s(aircraft.high_speed.eff_ttc)+" min")
print("")
print("Coût d'un voyage = "+"%.0f"%aircraft.economics.direct_operating_cost+" $")
# airplane 3D view
#------------------------------------------------------------------------------------------------------
print("-------------------------------------------")
print("3 view drawing : launched")
show.draw_3d_view(aircraft,"sequence packaged","This plane")
toc = ac.design_driver.top_of_climb_altp
oei_ceil_req = ac.low_speed.req_oei_altp
vz_clb, vz_crz, oei_path, oei_mach = perfo.ceilings(ac, toc, oei_ceil_req)
ac.high_speed.eff_vz_climb = vz_clb
ac.high_speed.eff_vz_cruise = vz_crz
ac.low_speed.eff_oei_path = oei_path
ac.low_speed.eff_oei_mach = oei_mach
delta_vz_clb = ac.high_speed.req_vz_climb - vz_clb
delta_vz_crz = ac.high_speed.req_vz_cruise - vz_crz
delta_oei_path = ac.low_speed.req_oei_path - oei_path
print('')
print('Constraint : delta_vz_clb = ', "%.2f" % unit.ftpmin_mps(delta_vz_clb),
'ft/min, (=< 0 ?)')
print('Constraint : delta_vz_crz = ', "%.2f" % unit.ftpmin_mps(delta_vz_crz),
'ft/min, (=< 0 ?)')
print('Constraint : delta_oei_path = ', "%.2f" % (delta_oei_path * 100),
'%, (=< 0 ?)')
# Time to climb to requested altitude
#------------------------------------------------------------------------------------------------------
toc = ac.high_speed.req_toc_altp
disa = 0
mass = ac.weights.mtow
vcas1 = ac.high_speed.cas1_ttc
vcas2 = ac.high_speed.cas2_ttc
mach = ac.design_driver.cruise_mach
print("Engine effective reference thrust = ","%.1f"%(aircraft.propulsion.reference_thrust_effective/10)," daN")
print("Wing area = ","%.1f"%aircraft.wing.area," m2")
print("")
print("Take off field length required = ","%.1f"%aircraft.low_speed.req_tofl," m")
print("Take off field length effective = ","%.1f"%aircraft.low_speed.eff_tofl," m")
print("")
print("Approach speed required = ","%.1f"%unit.kt_mps(aircraft.low_speed.req_app_speed)," kt")
print("Approach speed effective = ","%.1f"%unit.kt_mps(aircraft.low_speed.eff_app_speed)," kt")
print("")
#"""
print("Flight path required OEI = ","%.2f"%(aircraft.low_speed.req_oei_path*100)," %")
print("light path effective OEI = ","%.2f"%(aircraft.low_speed.eff_oei_path*100)," %")
print("")
print("Vertical speed required with MCL rating = ","%.1f"%unit.ftpmin_mps(aircraft.high_speed.req_vz_climb)," ft/min")
print("Vertical speed effective with MCL rating = ","%.1f"%unit.ftpmin_mps(aircraft.high_speed.eff_vz_climb)," ft/min")
print("")
print("Vertical speed required with MCR rating = ","%.1f"%unit.ftpmin_mps(aircraft.high_speed.req_vz_cruise)," ft/min")
print("Vertical speed effective with MCR rating = ","%.1f"%unit.ftpmin_mps(aircraft.high_speed.eff_vz_cruise)," ft/min")
print("")
print("Time to climb required = ","%.1f"%unit.min_s(aircraft.high_speed.req_ttc)," min")
print("Time to climb effective = ","%.1f"%unit.min_s(aircraft.high_speed.eff_ttc)," min")
# """
print("")
print("--------------------------------------------------------------")
print("MTOW = ","%.0f"%aircraft.weights.mtow," kg")
print("Cost mission fuel = ","%.1f"%aircraft.cost_mission.block_fuel," kg")
print("Cash Operating Cost = ","%.1f"%aircraft.economics.cash_operating_cost," $/trip")