Zobrazeno 1 - 10
of 62
pro vyhledávání: '"Michel van Tooren"'
Publikováno v:
Journal of Aircraft. 59:502-514
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba40d5b8c65398acdf4c3812d307b23e
https://doi.org/10.2514/1.c036481
https://doi.org/10.2514/1.c036481
Autor:
Michel van Tooren, Ali Elham
Publikováno v:
AIAA Journal. 52:320-337
A method for wing-shape optimization is presented, in which the wing outer shape is optimized not only for the best aerodynamic efficiency but also for the minimum structural weight. The so-called airfoil effective distance is used to capture the inf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c09c4aed492a04a3fa94486f4e4e3073
https://doi.org/10.2514/1.j052406
https://doi.org/10.2514/1.j052406
Publikováno v:
AIAA Journal. 51:2266-2277
A reliability-based optimization method under both aleatory and epistemic uncertainties is studied. The mixed uncertainties are analyzed by combined probability and evidence theory. If the mixed uncertainty analysis is directly embedded in reliabilit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d62df930c097c580ad9ba691599f4fb
https://doi.org/10.2514/1.j052327
https://doi.org/10.2514/1.j052327
Publikováno v:
Reliability Engineering & System Safety. 116:28-37
In engineering, there exist both aleatory uncertainties due to the inherent variation of the physical system and its operational environment, and epistemic uncertainties due to lack of knowledge and which can be reduced with the collection of more da
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9efd70b4e6d1bbcf298229d22ded4173
https://doi.org/10.1016/j.ress.2013.02.014
https://doi.org/10.1016/j.ress.2013.02.014
Publikováno v:
Acta Astronautica. 87:107-126
To assess the on-orbit servicing (OOS) paradigm and optimize its utilities by taking advantage of its inherent flexibility and responsiveness, the OOS system assessment and optimization methods based on lifecycle simulation under uncertainties are st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::456a8079e457a953cc95374aa55fe96b
https://doi.org/10.1016/j.actaastro.2013.02.005
https://doi.org/10.1016/j.actaastro.2013.02.005
Publikováno v:
Engineering Computations. 30:469-493
PurposeAn aerodynamic shape optimization algorithm is presented, which includes all aspects of the design process: parameterization, flow computation and optimization. The purpose of this paper is to show that the Class‐Shape‐Refinement‐Transfo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::811b48c4128ce71972cdc6328b6d1a44
https://doi.org/10.1108/02644401311329334
https://doi.org/10.1108/02644401311329334
Publikováno v:
Structural and Multidisciplinary Optimization. 48:339-354
To address the reliability-based multidisciplinary design optimization (RBMDO) problem under mixed aleatory and epistemic uncertainties, an RBMDO procedure is proposed in this paper based on combined probability and evidence theory. The existing dete
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3c6056be54df12d31f31c72ed1635ccf
https://doi.org/10.1007/s00158-013-0901-1
https://doi.org/10.1007/s00158-013-0901-1
Multidisciplinary Design Optimization supported by Knowledge Based Engineering supports engineers confronting this daunting and new design paradigm. It describes methodology for conducting a system design in a systematic and rigorous manner that supp
Autor:
Michel van Tooren, M.H. Straathof
Publikováno v:
Journal of Aircraft. 49:1091-1100
This paper will demonstrate the potential of the class-shape-refinement-transformation (CSRT) method for aerodynamically optimizing three-dimensional surfaces. The CSRTmethodwas coupled to an in-house Euler solver and this combination was used in an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc5fd918a7b356ee490b525fc64af80a
https://doi.org/10.2514/1.c031594
https://doi.org/10.2514/1.c031594
Autor:
Durk Steenhuizen, Michel van Tooren
Publikováno v:
Advanced Engineering Informatics
In the field of aerospace engineering currently a lot of research effort is directed towards the reduction of cruise drag of civil transport aircraft in order to reduce fuel burn, and hence environmental impact and costs. In order to reduce cruise dr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ff467f1ceeed824a85426b1004e989d3