The art of spacecraft design: A multidisciplinary challenge [PDF]
Actual design turn-around time has become shorter due to the use of optimization techniques which have been introduced into the design process. It seems that what, how and when to use these optimization techniques may be the key factor for future ...
Abdi, F. +3 more
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Aerodynamic design using numerical optimization [PDF]
The procedure of using numerical optimization methods coupled with computational fluid dynamic (CFD) codes for the development of an aerodynamic design is examined.
Chapman, G. T., Murman, E. M.
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Numerical optimization design of advanced transonic wing configurations [PDF]
A computationally efficient and versatile technique for use in the design of advanced transonic wing configurations has been developed. A reliable and fast transonic wing flow-field analysis program, TWING, has been coupled with a modified quasi-Newton ...
Cosentino, G. B., Holst, T. L.
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High-fidelity Multidisciplinary Sensitivity Analysis and Design Optimization for Rotorcraft Applications [PDF]
A multidisciplinary sensitivity analysis of rotorcraft simulations involving tightly coupled high-fidelity computational fluid dynamics and comprehensive analysis solvers is presented and evaluated.
Bauchau, Olivier A. +4 more
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The case for aerodynamic sensitivity analysis [PDF]
No specific solutions are offered, nor verified by applications, for its subject problem which is sensitivity analysis in Computational Fluid Dynamics (CFD).
Sobieszczanski-Sobieski, Jaroslaw
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On simple aerodynamic sensitivity derivatives for use in interdisciplinary optimization [PDF]
Low-aspect-ratio and piston aerodynamic theories are reviewed as to their use in developing aerodynamic sensitivity derivatives for use in multidisciplinary optimization applications.
Doggett, Robert V., Jr.
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Aerodynamic design and analysis of the AST-200 supersonic transport configuration concept [PDF]
The design and analysis of a supersonic transport configuration was conducted using linear theory methods in conjunction with appropriate constraints. Wing optimization centered on the determination of the required twist and camber and proper integration
Martin, G. L., Walkley, K. B.
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ASTROS: A multidisciplinary automated structural design tool [PDF]
ASTROS (Automated Structural Optimization System) is a finite-element-based multidisciplinary structural optimization procedure developed under Air Force sponsorship to perform automated preliminary structural design. The design task is the determination
Neill, D. J.
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Design and Verification of New Head Type of Super High-speed EMUs
机车电传动, 2016 To decrease the aerodynamic drag of super high-speed EMUs, integrating high-speed EMUs head type design elements at home and abroad together, a new head type for super high-speed EMUs with speed of 500 km/h was designed.
LI Ming, LI Minggao, LIU Nan, HAN Lu
doaj
Application of direct inverse analogy method (DIVA) and viscous design optimization techniques [PDF]
A direct-inverse approach to the transonic design problem was presented in its initial state at the First International Conference on Inverse Design Concepts and Optimization in Engineering Sciences (ICIDES-1).
Forbrich, D., Greff, E., Schwarten, H.
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