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Introduction and Scope
41 other sections not shown
acceleration addition adequate aerodynamic heating aeroelastic air inlet airflow airframe airplane airport altitude anticipated areas autoignition autoignition temperature automatic cabin cabin pressure capability climb components Conclusion configurations considerable control systems cooling critical cruising altitude deceleration delta wing descent duct system effect elevated temperature engine compartment engine failure environmental equipment established factors fatigue Federal Aviation Agency fire flight characteristics flight profile friction band functioning fuselage gradient hazards increased indicates landing distance limit load Mach number maintenance malfunction maneuver maximum nautical miles navigational necessary needed noise nozzle performance pilot possible pressure problem procedures propulsion system range reduce reliability rudder force runway safety satisfactory sonic boom sonic transport specific specific fuel consumption stability stall speed stickforce structural subsonic aircraft subsonic flight subsonic transport super supersonic aircraft supersonic flight supersonic speeds takeoff and landing thermal thrust transonic trim turbine variable geometry Variable Geometry Wings