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我要沮丧

Combined Optimization and Inverse Design of 3-D Aerodynamic Shapes, calls to a 3-D flow-field analysis code. Since certain general 3-D aerodynamic shape inverse design methodologies require only a few calls to a modified 3-D flow-field analysis code, it would be highly desirable to create a hybrid new design algorithm that would combine some of the best features of

LANCE

谈判

Ingratiate

Multidisciplinary Inverse Design and Optimization (MIDO),quence of uncoupled, single-discipline analyses involving flow field, temperature field, stress-strain field, structural dynamics, manufacturability tradeoffs and a large amount of personal designer’s experience and intuition [289]–[295]. Since the entire aircraft system is seemingly highly coupled,

NIB

Supersonic Aircraft Shape Optimization, will introduce a general approach to aerodynamic shape design based on minimization of energy consumption during aircraft life while considering realistic constraints on lift, pitching and rolling moments and geometric dimensions. The analysis is performed using a potential code with real flow corr

HIKE

famine

Laminar Flow for Supersonic Transports,isite to achieve very long range capability. In earlier studies it was assumed that SCTs would only become possible by application of laminar flow [376]. But today, we request an SCT to be viable without application of laminar flow in order to maintain its competitiveness when laminar flow becomes a

finale

The Oblique Flying Wing Transport,aft design teams around the world have not been successful at designing a ‘Concorde’ type large long range supersonic transport with realistic technology assumptions. It therefore seems only natural to look for other configurations that might fullfil this specification. The oblique flying wing confi

Exterior

Expostulate