@article{(Open Science Index):https://publications.waset.org/pdf/10008474,
	  title     = {Aerodynamic Coefficients Prediction from Minimum Computation Combinations Using OpenVSP Software},
	  author    = {Marine Segui and  Ruxandra Mihaela Botez},
	  country	= {},
	  institution	= {},
	  abstract     = {OpenVSP is an aerodynamic solver developed by National Aeronautics and Space Administration (NASA) that allows building a reliable model of an aircraft. This software performs an aerodynamic simulation according to the angle of attack of the aircraft makes between the incoming airstream, and its speed. A reliable aerodynamic model of the Cessna Citation X was designed but it required a lot of computation time. As a consequence, a prediction method was established that allowed predicting lift and drag coefficients for all Mach numbers and for all angles of attack, exclusively for stall conditions, from a computation of three angles of attack and only one Mach number. Aerodynamic coefficients given by the prediction method for a Cessna Citation X model were finally compared with aerodynamics coefficients obtained using a complete OpenVSP study.
	    journal   = {International Journal of Mechanical and Industrial Engineering},
	  volume    = {12},
	  number    = {1},
	  year      = {2018},
	  pages     = {9 - 16},
	  ee        = {https://publications.waset.org/pdf/10008474},
	  url   	= {https://publications.waset.org/vol/133},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 133, 2018},