Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
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This paper presents a theoretically and practically grounded architecture of design methods combination. A possibility and completeness of developing integral design solutions and intensifying the design process are provided by redistribution of emphases of numerical and natural experiments.
Keywordsmethod aerodynamic design aircraft integrated embodiment submerged air intake propulsion system numerical experiment natural experiment wind tunnel model identification
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