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A Dynamic Calibration Method for Experimental and Analytical Hub Load ComparisonThis paper presents the results from an ongoing effort to produce improved correlation between analytical hub force and moment prediction and those measured during wind-tunnel testing on the Aeroelastic Rotor Experimental System (ARES), a conventional rotor testbed commonly used at the Langley Transonic Dynamics Tunnel (TDT). A frequency-dependent transformation between loads at the rotor hub and outputs of the testbed balance is produced from frequency response functions measured during vibration testing of the system. The resulting transformation is used as a dynamic calibration of the balance to transform hub loads predicted by comprehensive analysis into predicted balance outputs. In addition to detailing the transformation process, this paper also presents a set of wind-tunnel test cases, with comparisons between the measured balance outputs and transformed predictions from the comprehensive analysis code CAMRAD II. The modal response of the testbed is discussed and compared to a detailed finite-element model. Results reveal that the modal response of the testbed exhibits a number of characteristics that make accurate dynamic balance predictions challenging, even with the use of the balance transformation.
Document ID
20170004507
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kreshock, Andrew R.
(Army Research Lab. Hampton, VA, United States)
Thornburgh, Robert P.
(Army Research Lab. Hampton, VA, United States)
Wilbur, Matthew L.
(Army Research Lab. Hampton, VA, United States)
Date Acquired
May 9, 2017
Publication Date
March 1, 2017
Subject Category
Structural Mechanics
Aircraft Stability And Control
Report/Patent Number
ARL-RP-0592
NF1676L-25065
NASA/TM-2017-219601
L-20736
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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