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the configuration layout of a Gulfstream IV and you now havea The other associated parameters are You design team has completed layout ofa better gross weight estimate of Wo-73 summarized below: Fuel weight W, = 295001b Aspect ratio AR 5.92 Planform area S 950 ft Oswald efficiency e-0.9 Zero-lift drag coefficient Cpo 0.015 Wing height above ground h = 6 ft Twin Rolls-Royce Tay 611-S turbofan engines, Tusx -13,850tb each (sea level) Thrust specific fuel consumption G = 0.69 lb / (lb·hr)
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