Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis

Ghoreyshi, M., Badcock, K. J., Da Ronch, A., Marques, S., Swift, A. and Ames, N. (2011) Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis. Journal of Aircraft, 48 (1), 42-55. (doi:10.2514/1.C001003).

Abstract

This paper describes the use of the Euler equations for the generation and testing of tabular aerodynamic models for flight dynamics analysis. Maneuvers for the AGARD Standard Dynamics Model sharp leading-edge wind-tunnel geometry are considered as a test case. Wind-tunnel data is first used to validate the prediction of static and dynamic coefficients at both low and high angles, featuring complex vortical flow, with good agreement obtained at low to moderate angles of attack. Then the generation of aerodynamic tables is described based on a data fusion approach. Time-optimal maneuvers are generated based on these tables, including level
flight trim, pull-ups at constant and varying incidence, and level and 90 deg turns. The maneuver definition includes the aircraft states and also the control deflections to achieve the motion. The main point of the paper is then to assess the validity of the aerodynamic tables which were used to define the maneuvers. This is done by replaying them, including the control surface motions, through the time accurate computational fluid dynamics code. The resulting forces and moments are compared with the tabular values to assess the presence of inadequately modeled dynamic or unsteady effects. The agreement between the tables and the replay is demonstrated for slow maneuvers. Increasing rate maneuvers show discrepancies which are ascribed to vortical
flow hysteresis at the higher rate motions. The framework is suitable for application to more complex viscous
flow models, and is powerful for the assessment of the validity of aerodynamics models of the type currently used for studies of flight dynamics.

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Contributors

Author: A. Da Ronch

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