%0 Journal Article
	%A M. Rychlik and  R. Roszak and  M. Morzynski and  M. Nowak and  H. Hausa and  K. Kotecki
	%D 2012
	%J International Journal of Structural and Construction Engineering
	%B World Academy of Science, Engineering and Technology
	%I Open Science Index 67, 2012
	%T Preparation of Computer Model of the Aircraft for Numerical Aeroelasticity Tests – Flutter
	%U https://publications.waset.org/pdf/2042
	%V 67
	%X Article presents the geometry and structure
reconstruction procedure of the aircraft model for flatter research
(based on the I22-IRYDA aircraft). For reconstruction the Reverse
Engineering techniques and advanced surface modeling CAD tools
are used. Authors discuss all stages of data acquisition process,
computation and analysis of measured data. For acquisition the three
dimensional structured light scanner was used. In the further sections,
details of reconstruction process are present. Geometry
reconstruction procedure transform measured input data (points
cloud) into the three dimensional parametric computer model
(NURBS solid model) which is compatible with CAD systems.
Parallel to the geometry of the aircraft, the internal structure
(structural model) are extracted and modeled. In last chapter the
evaluation of obtained models are discussed.
	%P 1136 - 1142