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CONFIGURATION DESIGN ANALYSIS
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60 PASSENGER TILT 60-passenger aerodynamic airplane airstairs Area sq ft Auxiliary Power Unit blade Block Distance blown flap Boeing Boeing Company bypass ratio cabin CHARACTERISTICS SUMMARY climb CN CN configuration control power control system critical engine cruise engines design gross weight Direct Operating Costs duct Equipment equivalent airspeed Fan-in-Wing STOL feet flap Flight Controls gust sensitivity H CN increase Installation Jet Lift VTOL kts EAS lift coefficient lift engines Lift Fan VTOL lift propulsion load factor Long Pattern monocyclic control navigation systems nozzles payload percent performance pitch control pounds pressure ratio range Reaction Controls Revenue Cargo shown in Figure specific fuel consumption stage length statute miles STOL aircraft Stowed Rotor Table Tail Area sq takeoff and landing Tilt Wing VTOL tilt-wing trim True airspeed TT T TT TT TT turbine inlet temperature turbocompressors V/STOL VTOL WEIGHT weight penalty wing loading