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Hoogreef, M.F.M. (author), D'Ippolito, R. (author), Augustinus, R. (author), La Rocca, G. (author)
This paper presents the status of development of an MDO advisory system, coupled to an optimization configurator for a process integration and design optimization (PIDO) system. This advisory system can support non-experts in the application of MDO by giving advice on the type of MDO architecture to use and assist in the implementation of the...
conference paper 2015
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Hoogreef, M.F.M. (author), La Rocca, G. (author)
Multidisciplinary Design Optimization (MDO) can aid designers to improve already mature design solutions, as well as to explore innovative, complex engineering products. It is a methodology, complete with mathematical formulations, that assists in the optimization of a complex product, whilst considering and exploiting discipline interactions....
conference paper 2015
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Hoogreef, M.F.M. (author), Van Dijk, R.E.C. (author), La Rocca, G. (author), d'Ippolito, R. (author)
The Product Development Process (PDP) of manufacturing companies requires the efficient management of huge amounts of data from different sources and their integration in the sub-processes that compose the product development chain. This is a very challenging endeavor for which an integrated approach does not yet exist. The EC FP7 Project iProd...
conference paper 2014
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Vos, R. (author), Hoogreef, M.F.M. (author)
This paper presents a semi-analytical method for the weight estimation of fuselages with an oval cross-section, applied to blended wing body aircraft. The weight estimation of the fuselage primary structure is based on a structural analysis of two-dimensional crosssections and it is completed by a set of empirical relations for the weight...
conference paper 2013
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Vos, R. (author), Geuskens, F.J.J.M.M. (author), Hoogreef, M.F.M. (author)
This paper outlines a new concept for a pressure cabin design for blended-wing-body aircraft. An overview is presented of the wide oval cabin and why it is believed to be a possible alternative to existing designs of non-circular pressurized cabins. The perimeter of the oval cross section is formed by four smoothly connecting arcs of different...
conference paper 2012
Searched for: department%3A%22Aerodynamics%252C%255C%252BWind%255C%252BEnergy%255C%252B%2526%255C%252BPropulsion%22
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