NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Calibration and Data Analysis Recommendations for Three-Component Moment BalancesFundamental characteristics of design, calibration, and application of three-component moment balances are investigated in great detail. These balances are typically used to determine loads on control surfaces, canards, or other parts that are attached to a wind tunnel model. First, three different descriptions of the load state of a moment balance are reviewed. Then, load transformations between different load formats and the combined load diagram for two of the three load components are discussed. An error analysis showed that it is critical to maximize the product of the distance between the bending moment gages and their sensitivities in order to minimize the overall error in the normal force prediction. In addition, it is important to apply a sufficient number of calibration loadings near the first bending moment gage. Then, unwanted near-linear dependencies between the two bending moment gage outputs can be avoided. The error in the bending moment prediction is also investigated that results from the elastic deformation of the metric part of the balance under load. Finally, the application of the Non-Iterative Method to three-component moment balance calibration data is described in order to obtain regression models that can be used to predict loads from measured outputs during a wind tunnel test.
Document ID
20190026534
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ulbrich, N.
(Jacobs Engineering Group Mountain View, CA, United States)
Reed, M.
(Aerodyne Industries, LLC Houston, TX, United States)
Date Acquired
June 20, 2019
Publication Date
June 17, 2019
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
ARC-E-DAA-TN66180
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum (Aviation 2019)
Location: Dallas, TX
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNA16BD26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Strain-Gage Balance
Wind Tunnel Tests
No Preview Available