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Commenced in January 2007 Frequency: Monthly Edition: International Publications Count: 30172


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10008474
Aerodynamic Coefficients Prediction from Minimum Computation Combinations Using OpenVSP Software
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.
Digital Object Identifier (DOI):

References:

[1] C. Footprint. Calculatrice du Bilan Carbone des Vols Available: ttp://calculator.carbonfootprint.com
[2] I. Secretariat, "Aviation’s Contribution to Climate Change," BAN Ki-Moon, 2010.
[3] A. Hamy, A. Murrieta-Mendoza, and R. Botez, "Flight Trajectory Optimization to Reduce Fuel Burn and Polluting Emissions using a Performance Database and Ant Colony Optimization Algorithm," 2016.
[4] A. Murrieta Mendoza, C. Romain, and R. Botez, "3D reference trajectory optimization for a commercial aircraft using a graph search algorithm," 2016.
[5] A. Murrieta-Mendoza, J. Gagné, and R. M. Botez, "GRIB2 weather extraction and use for flight optimization algorithms," in Sustainability 2015-An International Conference on Environmental Sustainability in Air Vehicle Design and Operations of Helicopters and Airplane, 2015.
[6] A. Murrieta-Mendoza, J. Gagné, and R. M. Botez, "New search space reduction algorithm for vertical reference trajectory optimization," INCAS Bulletin, vol. 8, p. 77, 2016.
[7] A. Murrieta-Mendoza, H. Ruiz, R. M. Botez, and T. Supérieure, "Vertical Reference Flight Trajectory Optimization with the Particle Swarm Optimisation," in The 36th IASTED International Conference on Modelling, Identification and Control (MIC 2017). Innsbrunck, Austria, 2017.
[8] A. Murrieta-Mendoza, H. Ruiz, S. Kessaci, and R. M. Botez, "3D Reference Trajectory Optimization Using Particle Swarm Optimization," in 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017, p. 3435.
[9] R. S. Félix Patrón, Y. Berrou, and R. M. Botez, "Climb, Cruise and Descent 3D Trajectory Optimization Algorithm for a Flight Management System," in Aviation Technology, Integration, and Operations, 2014.
[10] R. S. Félix Patrón and R. M. Botez, "Flight trajectory optimization through genetic algorithms coupling vertical and lateral profiles," in ASME 2014 International Mechanical Engineering Congress and Exposition, 2014, pp. V001T01A048-V001T01A048.
[11] R. S. Félix Patrón, A. Kessaci, and R. M. Botez, "Horizontal Flight Trajectories Optimization for Commercial Aircraft through a Flight Management System," Aeronautical Journal, vol. 118, 2014.
[12] R. S. Félix Patrón, A. Kessaci, R. M. Botez, and D. Labour, "Flight trajectories optimization under the influence of winds using genetic algorithms," in AIAA Guidance, Navigation, and Control (GNC) Conference, 2013.
[13] O. Ş. Gabor, A. Koreaschi, R. M. Botez, M. Mamou, and Y. Mebarki, "Analysis of the Aerodynamic Performance of a Morphing Wing-Tip Demonstrator Using a Novel Nonlinear Vortex Lattice Method," 2016.
[14] A. Koreanschi, O. Ş. Gabor, T. Ayrault, R. M. Botez, M. Mamou, and Y. Mebarki, "Numerical Optimization and Experimental Testing of a Morphing Wing with Aileron System," in 24th AIAA/AHS Adaptive Structures Conference, 2016, p. 1083.
[15] O. Gabor Sugar, A. Koreanschi, and R. M. Botez, "A New Non-Linear Vortex Lattice Method: Applications to Wing Aerodynamic Optimizations," Chinese Journal of Aeronautics, vol. 29, pp. 1178-1195, 2016.
[16] J. Byrne, P. Cardiff, and A. Brabazon, "Evolving Parametric Aircraft Models for Design Exploration and Optimisation," Neurocomputing, vol. 142, pp. 39-47, 2014.
[17] A. M. Gary and R. A. McDonald, "Parametric Identification of Surface Regions in OpenVSP for Improved Engineering Analysis," in 53rd AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics, Kissimmee, FL, 2015, pp. 1-13.
[18] J. R. Gloudemans and R. A. McDonald, "User Defined Components in the OpenVSP Parametric Geometry Tool," in 15th AIAA Aviation Technology, Integration, and Operations Conference, American Institute of Aeronautics and Astronautics, Dallas, TX, 2015, pp. 1-7.
[19] R. A. McDonald, "Interactive Reconstruction of 3D Models in the OpenVSP Parametric Geometry Tool," in 53rd AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics, Kissimmee, FL, 2015, pp. 1-10.
[20] R. M. Botez, C. Hamel, G. Ghazi, Y. Boughari, F. Theel, and A. Murrieta Mendoza, "Level D Research Aircraft Flight Simulator use for Novel Methodologies in Aircraft Modeling and Simulation," 2015.
[21] M. Segui, M. Kuitche, R. M. Botez, and O. Sugar-Gabor, "Longitudinal aerodynamic coefficients of hydra technologies UAS-S4 from geometrical data," in Proceedings of AIAA Modeling and Simulation Technologies Conference, AIAA SciTech Forum 2017, 2017.
[22] B. Etkin and L. D. Reid, Dynamics of flight: stability and control vol. 3: Wiley New York, 1996.

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