Copyright © 2016 by the American Institute of Aeronautics and AstronauticsMorote, J.Liaño, GabrielJiménez-Varona, José2026-02-192026-02-192017-01-31Journal of Spacecraft and Rockets 54(2)0022-4650https://arc.aiaa.org/doi/10.2514/1.A33764https://hdl.handle.net/20.500.12666/1731A theoretical investigation of the rolling motion of triform configurations at high angles of attack is presented. A nonlinear aerodynamic flow model, derived from strip and slender body theories, is used to predict the aerodynamic roll coefficients of triform tailed missiles at high angles of attack. The flow model predictions are compared to the estimates of a panel-based code and a computational fluid dynamics code at two Mach numbers.engMissilesAngle of AttackAeropredictionSlender body theoryComputational fluid dynamics codeAerodynamic flowsFluentVortex sheddingTurbulence modelsSubsonic velocityinfo:eu-repo/semantics/article10.2514/1.A337641533-6794info:eu-repo/semantics/restrictedAccess