A new efficient technology of aerodynamic design based on CFD driven optimization

Epstein, Boris; Peigin, S. V.; Tsach, Shlomo

doi:10.1016/j.ast.2005.11.001

Cited by 14 publications

(4 citation statements)

References 9 publications

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“…A detailed analysis shows that this is attributed to a successful shock destruction which allowed to eliminate most of the wave drag. More details may be found in [18] (RAE2822) and in [28] (ONERA M6).…”

Section: Verification Studiesmentioning

confidence: 99%

Accurate CFD driven optimization of lifting surfaces for wing-body configuration

Epstein

Peigin

2007

Computers & Fluids

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Section: Verification Studiesmentioning

confidence: 99%

Accurate CFD driven optimization of lifting surfaces for wing-body configuration

Epstein

Peigin

2007

Computers & Fluids

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“…Novel complex geometries are generally constructed manually which is very time consuming. 35 In order to overcome this automatic mesh constructions are required. CFD ultimately restricts the allowable design space either through computational needs or through how the baseline geometry is allowed to deform with a fixed mesh.…”

Section: Model Descriptionmentioning

confidence: 99%

Aerodynamic Optimisation of Non-planar Lifting Surfaces

Skinner

Zare‐Behtash

2016

57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

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A novel population structured genetic algorithm (sGA) with embedded potential flow vortex ring panel method (VRM) has been developed to minimise induced and parasitic drag subject to constraints on lift, root bending moment, and longitudinal static stability. The optimisation architecture can activate up to four independent wing segments allowing up to 28 design variables. Minimum drag of wing tip extensions and winglet configurations are compared using the non-linear stochastic optimisation method. The optimiser identified joined box wings as offering the greatest induced efficiency followed by C-wings. With span and root bending moment constraints winglets offered best total drag reduction. C-wings are further investigated for potential to enhance longitudinal static stability performance by staggering the horizontal extension of the winglet to balance moments around the wing's centre of gravity. Preliminary results suggest that while longitudinal static stability can be reached it would be very poor. Inclusion of more design constraints and additional analysis of the structural dynamics of C-wings, especially effecting the torsional mode, is necessary.

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“…Risk assessment and reliability design is an engineering approach widely used for solving system design problems in other fields in which the performed function is important, such as nuclear facilities [29], aerospace [30] and automobile [31] industry, building structures [32], powers systems [33], etc. In this paper, an extension of the reliability-based design approach to the hygrothemal building design is developed.…”

Section: Hygrothermal Comfort Reliability and Discomfort Riskmentioning

confidence: 99%

Comfort reliability evaluation of building designs by stochastic hygrothermal simulation

Sulaiman

Olsina

2014

Renewable and Sustainable Energy Reviews

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A new efficient technology of aerodynamic design based on CFD driven optimization

Cited by 14 publications

References 9 publications

Accurate CFD driven optimization of lifting surfaces for wing-body configuration

Accurate CFD driven optimization of lifting surfaces for wing-body configuration

Aerodynamic Optimisation of Non-planar Lifting Surfaces

Comfort reliability evaluation of building designs by stochastic hygrothermal simulation

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