Modelling transverse gusts using pitching, plunging and surging airfoil motions
Modelling transverse gusts using pitching, plunging and surging airfoil motions
Three model-motions were developed to replicate the aerodynamic response of a transverse gust. These motions included a pure-plunging and two three degree-of-freedom motions that approximated the angle-of-attack distribution produced by the gust. Using inviscid models and viscous flow simulations, the response of the gust and model-motions were compared as a function of the non-dimensional reduced frequency. The inviscid model was found to overestimate the influence of the rotational added-mass in the three degree-of-freedom motions. In contrast, the viscous flow simulations showed that the two primary sources of discrepancy between the gust and model-motions lie in the non-linear angle-of-attack distribution caused by the gust, and the wake development during the model-motions. Flow simulations showed that all three motions experienced greater than 90% agreement in lift for gusts with reduced frequencies less than 0.5, indicating that under this reduced frequency: 1) the effect of the gust convection is minimal; and 2) a pure-plunging motion may suffice for modelling gusts. However, at higher reduced frequencies the pure-plunging motion experiences greater than 10% worse agreement than the three degree-of-freedom motions. Overall, the motions provide a good approximation with greater than 90% accuracy in lift for gusts of reduced frequencies less than k = 0.75.
Leung, Jordan
2fd99b87-5fa1-4abc-bf11-a914a5995554
Wong, Jamie
64ffa4d3-f209-407e-8f05-fb7372d325fd
Weymouth, Gabriel
b0c85fda-dfed-44da-8cc4-9e0cc88e2ca0
Rival, David
a2e24ff6-d135-4c51-ac7a-7c8877a18f5d
Leung, Jordan
2fd99b87-5fa1-4abc-bf11-a914a5995554
Wong, Jamie
64ffa4d3-f209-407e-8f05-fb7372d325fd
Weymouth, Gabriel
b0c85fda-dfed-44da-8cc4-9e0cc88e2ca0
Rival, David
a2e24ff6-d135-4c51-ac7a-7c8877a18f5d
Leung, Jordan, Wong, Jamie, Weymouth, Gabriel and Rival, David
(2018)
Modelling transverse gusts using pitching, plunging and surging airfoil motions.
AIAA Journal.
(doi:10.2514/1.J056961).
Abstract
Three model-motions were developed to replicate the aerodynamic response of a transverse gust. These motions included a pure-plunging and two three degree-of-freedom motions that approximated the angle-of-attack distribution produced by the gust. Using inviscid models and viscous flow simulations, the response of the gust and model-motions were compared as a function of the non-dimensional reduced frequency. The inviscid model was found to overestimate the influence of the rotational added-mass in the three degree-of-freedom motions. In contrast, the viscous flow simulations showed that the two primary sources of discrepancy between the gust and model-motions lie in the non-linear angle-of-attack distribution caused by the gust, and the wake development during the model-motions. Flow simulations showed that all three motions experienced greater than 90% agreement in lift for gusts with reduced frequencies less than 0.5, indicating that under this reduced frequency: 1) the effect of the gust convection is minimal; and 2) a pure-plunging motion may suffice for modelling gusts. However, at higher reduced frequencies the pure-plunging motion experiences greater than 10% worse agreement than the three degree-of-freedom motions. Overall, the motions provide a good approximation with greater than 90% accuracy in lift for gusts of reduced frequencies less than k = 0.75.
Text
Leung_Wong_Weymouth_Rival_AIAA_Manuscript
- Accepted Manuscript
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Accepted/In Press date: 17 April 2018
e-pub ahead of print date: 31 May 2018
Identifiers
Local EPrints ID: 421633
URI: http://eprints.soton.ac.uk/id/eprint/421633
ISSN: 0001-1452
PURE UUID: 1d02429d-4335-4d57-94d6-7f22718c688f
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Date deposited: 18 Jun 2018 16:30
Last modified: 16 Mar 2024 04:15
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Author:
Jordan Leung
Author:
Jamie Wong
Author:
David Rival
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