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Assessment of Sting Effect on X-31 Aircraft Model Using CFD
2010
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
unpublished
The article describes the computational evaluation of the effect a belly mounted sting on the aerodynamics characteristics of an X-31 wind tunnel model. The investigation includes results of steady and time-dependent CFD analysis of the X-31 model with and without sting. The values of the steady lift and pitching moment coefficients as well as the pitching moment of model undergoing a manuever are compared to each other and to the wind tunnel data. The results of this analysis show the
doi:10.2514/6.2010-1040
fatcat:d7ew2rp7xrcsxnnq4a4if6crm4