Evaluation of Cryogenic Force Balance Calibration Methodologies Relative to Wind Tunnel Results-Reference-Cited by-同舟云学术

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Evaluation of Cryogenic Force Balance Calibration Methodologies Relative to Wind Tunnel Results

Published:2019-07 Issue:4 Volume:56 Page:1398-1406
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Burns Devin E.,Toro Kenneth G.,Parker Peter A.,Melissa Rivers S.,Quix Harald,Wright Martin

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035211

Reference7 articles.

1. FerrisA. J. “Strain Gauge Balance Calibration and Data Reduction at NASA Langley Research Center,” First International Symposium on Strain Gauge Balances, NASA CP-1999-209101/PT2, 1999, pp. 565–572.

2. Cryogenic balance technology at the National Transonic Facility

3. A new and working automatic calibration machine for wind tunnel internal force balances

4. Experimental Investigations of the NASA Common Research Model (Invited)

5. Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited)

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An Improved High-Capacity Balance Calibration Methodology;IEEE Sensors Journal;2024-01-01

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