Evaluation of dynamic derivatives using computational fluid dynamics
Evaluation of dynamic derivatives using computational fluid dynamics
This paper focuses on the evaluation of the dynamic stability derivative formulation. The derivatives are calculated using the Euler and Reynolds-averaged Navier–Stokes equations, and a time-domain solver was used for the computation of aerodynamic loads for forced periodic motions. To validate the predictions, two test cases are used. For the standard dynamic model geometry, a database of dynamic simulations illustrates the effects of the systematic variation of motion and fluid parameters involved. A satisfactory agreement was observed with available experimental data, and the dependency of dynamic derivatives on a number of parameters, such as Mach number, mean angle of attack, frequency, and amplitude, was assessed. For the transonic cruiser wind-tunnel geometry, static and unsteady aerodynamic characteristics were validated against experimental measurements. The ability of models based on the dynamic derivatives to predict large-amplitude motion forces and moments was assessed. It was demonstrated that the dynamic derivative model does not represent all of the important effects due to aerodynamics.
470-484
Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Vallespin, D.
b979d052-a22b-4b46-8578-2fb851b7e174
Ghoreyshi, M.
e43d6179-9d81-4c53-9057-9c7f8ec588fb
Badcock, K. J.
64c4dc5d-1f2f-4358-af31-f6506c1810ef
February 2012
Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Vallespin, D.
b979d052-a22b-4b46-8578-2fb851b7e174
Ghoreyshi, M.
e43d6179-9d81-4c53-9057-9c7f8ec588fb
Badcock, K. J.
64c4dc5d-1f2f-4358-af31-f6506c1810ef
Da Ronch, A., Vallespin, D., Ghoreyshi, M. and Badcock, K. J.
(2012)
Evaluation of dynamic derivatives using computational fluid dynamics.
AIAA Journal, 50 (2), .
(doi:10.2514/1.J051304).
Abstract
This paper focuses on the evaluation of the dynamic stability derivative formulation. The derivatives are calculated using the Euler and Reynolds-averaged Navier–Stokes equations, and a time-domain solver was used for the computation of aerodynamic loads for forced periodic motions. To validate the predictions, two test cases are used. For the standard dynamic model geometry, a database of dynamic simulations illustrates the effects of the systematic variation of motion and fluid parameters involved. A satisfactory agreement was observed with available experimental data, and the dependency of dynamic derivatives on a number of parameters, such as Mach number, mean angle of attack, frequency, and amplitude, was assessed. For the transonic cruiser wind-tunnel geometry, static and unsteady aerodynamic characteristics were validated against experimental measurements. The ability of models based on the dynamic derivatives to predict large-amplitude motion forces and moments was assessed. It was demonstrated that the dynamic derivative model does not represent all of the important effects due to aerodynamics.
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Published date: February 2012
Organisations:
Aerodynamics & Flight Mechanics Group
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Local EPrints ID: 351516
URI: http://eprints.soton.ac.uk/id/eprint/351516
ISSN: 0001-1452
PURE UUID: 4528337a-1f40-4f35-9953-d019f1af1a22
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Date deposited: 23 Apr 2013 12:30
Last modified: 15 Mar 2024 03:46
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Author:
D. Vallespin
Author:
M. Ghoreyshi
Author:
K. J. Badcock
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