Information-Based Sensor Placement for Data-Driven Estimation of Unsteady Flows

被引:6
|
作者
Graff, John [1 ]
Medina, Albert [2 ]
Lagor, Francis D. [1 ]
机构
[1] SUNY Buffalo, Dept Mech & Aerosp Engn, Buffalo, NY 14260 USA
[2] US Air Force, Aerodynam Technol Branch, Aerosp Syst Directorate, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
Flow Conditions; Distributed Sensing; Stagnation Point; Kalman Filter; Airfoil Surface; Aerodynamic Performance; Pressure Sensors; Data Driven Model; Flight Vehicle; Proper Orthogonal Decomposition; NONLINEAR-SYSTEMS; DYNAMICAL-SYSTEMS; SELECTION; DECOMPOSITION;
D O I
10.2514/1.J063015
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Estimation of unsteady flowfields around flight vehicles may improve flow interactions and lead to enhanced vehicle performance. Although flowfield representations can be very high-dimensional, their dynamics can sometimes have low-order representations that may be estimated using a few, appropriately placed measurements. This paper presents a sensor-selection framework for the intended application of data-driven, flowfield estimation. This framework combines data-driven modeling, steady-state Kalman filter design, and sparse, sequential sensor selection. This paper also uses the sensor selection framework to design sensor arrays that can perform well for a collection of operating conditions. Flow estimation results on numerical data show that the proposed framework produces arrays that are highly effective at flowfield estimation for the flow behind and an airfoil at a high angle of attack using embedded pressure sensors. Analysis of the flowfields reveals that paths of impinging stagnation points along the airfoil's surface during a shedding period of the flow are highly informative locations for placement of pressure sensors.
引用
收藏
页码:4864 / 4878
页数:15
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