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LikeSNU에서 의미기반으로 분석하여 연관된 자료를 추천해드립니다.
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Characteristics of thin triangular wings with constant - chord full - span control surfaces at supersonic speeds
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Design and Development of Aerospace Vehicles and Propulsion Systems : Proceedings of SAROD 2018
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Wind - tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing - edge angles on a semispan wing model
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Energy efficiency in motor driven systems
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Structural integrity : theory and experiment
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수소생산 저장 액화 충전 수소연료전지 선박
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Scramjet propulsion
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Automotive NVH technology
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Generalized linearized conical flow
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Polymer composites in the aerospace industry
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Characteristics of thin triangular wings with triangular - tip control surfaces at supersonic speeds with mach lines behind the leading edge
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Investigation of suction - slot shapes for controlling a turbulent boundary layer
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Advanced aircraft design : conceptual design, analysis, and optimization of subsonic civil airplanes
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Aircraft propulsion
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Future propulsion systems and energy sources in sustainable aviation
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Aircraft propulsion and gas turbine engines
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Application of the linearized theory of supersonic flow to the estimation of control - surface characteristics
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Theoretical supersonic lift and drag characteristics of symmetrical wedge - shape - airfoil sections as affected by sweepback outside the mach cone
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Inlets for supersonic missiles
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Intake aerodynamics
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