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mirzaei, M., abbaszadeh, M., hoseini, I., Montazeri, M. (2024). Design of Optimal Arrangement for Improving Accuracy of Tilt Measurement Unit for Wind Tunnel Balance. Electronic and Cyber Defense, 13(1), 13-29.
mojtaba mirzaei; mohammad abbaszadeh; iman hoseini; Mohammad Hossein Montazeri. "Design of Optimal Arrangement for Improving Accuracy of Tilt Measurement Unit for Wind Tunnel Balance". Electronic and Cyber Defense, 13, 1, 2024, 13-29.
mirzaei, M., abbaszadeh, M., hoseini, I., Montazeri, M. (2024). 'Design of Optimal Arrangement for Improving Accuracy of Tilt Measurement Unit for Wind Tunnel Balance', Electronic and Cyber Defense, 13(1), pp. 13-29.
mirzaei, M., abbaszadeh, M., hoseini, I., Montazeri, M. Design of Optimal Arrangement for Improving Accuracy of Tilt Measurement Unit for Wind Tunnel Balance. Electronic and Cyber Defense, 2024; 13(1): 13-29.

Design of Optimal Arrangement for Improving Accuracy of Tilt Measurement Unit for Wind Tunnel Balance

مکانیک سیالات و آیرودینامیک
Article 2, Volume 13, Issue 1 - Serial Number 33, September 2024, Pages 13-29    PDF (1.78 M)
Document Type: Original Article
Authors
mojtaba mirzaei* 1; mohammad abbaszadeh2; iman hoseini2; Mohammad Hossein Montazeri2
1Associate Professor, Shiraz University, Shiraz, Iran
2Assistant Professor, Shiraz University, Shiraz, Iran
Receive Date: 02 March 2024,  Revise Date: 05 June 2024,  Accept Date: 23 June 2024 
Abstract
The wind tunnel is one of the most widely used equipment in the design of flight vehicles to investigate the control surface effectiveness and also, aerodynamic pre-flight behavior of these vehicles. On the other hand, one of the most essential parts of the wind tunnel is the balance tilt measurement unit, which measures the attitude of the balance and installed model with high accuracy. There are several ways to design the tilt measurement unit of wind tunnel balance. One of them is to use proper and efficient accelerometers by considering selection, and optimal installation of them in the tilt measurement unit of wind tunnel balance. These Considerations are necessary to reduce the measuring error and make the test results reliable. In this paper, firstly, the effective parameters and calibration methods will be presented. Then, several arrangement methods for installation of these accelerometers will be presented and finally, the optimal design method will be proposed.
Keywords
Wind Tunnel; Balance; Tilt Measurement Unit; Accelerometer; Calibration; Optimization
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