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Practical Considerations using Weighted-Acceleration Compensation Techniques for Dynamic Force Measurements in Wind TunnelsMost wind tunnel force measurement systems are designed and calibrated for high-accuracy static measurements, but may have limited ability to sense dynamic forces and moments. As a means to improve the measurement bandwidth of dynamic forces, researchers have proposed using a weighted-acceleration technique, which uses accelerometer data to compensate and correct for system dynamics. The sum of weighted-accelerations method is attractive as the acceleration data applies a correction to the traditional static measurements. The focus of this paper is on practical aspects of implementing a weighted-acceleration technique in an experimental arrangement. A formulation of the weighted-acceleration methodology is validated on a reduced-order model and demonstrated on a tabletop experiment that serves as a proxy to
a wind tunnel force measurement system. As part of this system, a two component normal force and pitching moment balance was designed and fabricated. A static and dynamic calibration of the system was performed, and the weighted-acceleration technique was used to reconstruct impact forces acting on the system. Practical considerations of the experimental design that improve the success of the methodology are discussed.
Document ID
20240014121
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
GarrettTrowbridge
(Pennsylvania State University State College, United States)
Nicholas Vlajic
(Applied Research Laboratory at Penn State State College, United States)
Devin Burns
(Langley Research Center Hampton, United States)
Date Acquired
November 7, 2024
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics AIAA
Funding Number(s)
WBS: 725017.02.07.03.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Dynamic force measurement
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