2012
DOI: 10.1260/1756-8293.4.1.79
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Modeling MAV Response in Gusty Urban Environment

Abstract: The article discusses an airfoil unsteady aerodynamic response to upstream unsteady flow disturbances in flow regimes characteristic of Micro Air Vehicle (MAV) applications. Because of their small size and speed, the flight control of these vehicles in gusty urban environments poses tremendous challenges addressed in the current work. Following a thorough review of experimental and numerical studies characterizing various scales and configurations of urban flow disturbances, three canonical gust models are pro… Show more

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Cited by 29 publications
(9 citation statements)
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“…MAVs are one of the largest groups that are vulnerable to gust loads due to their weakness in resisting gust loads (61,62,73,(158)(159)(160)(161)(162) . The flying speed of a MAV is around 10 to 20 m/s, which is at the same scale of the velocity of a normal gust.…”
Section: Aerodynamicsmentioning
confidence: 99%
“…MAVs are one of the largest groups that are vulnerable to gust loads due to their weakness in resisting gust loads (61,62,73,(158)(159)(160)(161)(162) . The flying speed of a MAV is around 10 to 20 m/s, which is at the same scale of the velocity of a normal gust.…”
Section: Aerodynamicsmentioning
confidence: 99%
“…One of the visible characteristics of urban environment is with the high and dense buildings, which may block the air flow and result in back flow. 24,25 That irregular vortex will change the air velocity. When the vortex and the air have the same/opposite direction of flow, the wind velocity will increase/decrease.…”
Section: Model Establishment Of the Delivery Task In Urban Environmentmentioning
confidence: 99%
“…The effects of synthetic-jet actuation are considered in application to unsteady flow over airfoils and analyzed using a high-accuracy compressible viscous ILES solver (Visbal & Gaitonde, 2002). FDL3DI (2015 version), is the updated solver used in our previous gust-airfoil and vortex-airfoil interaction studies (Golubev, Nguyen, & Visbal, 2010a;Golubev, & Visbal, 2012). In the numerical procedure, all variables are nondimensionalized by the airfoil chord and freestream flow density ∞ and flow velocity ∞ .…”
Section: Procedures Overviewmentioning
confidence: 99%