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Mathematical Simulation and Experimental Investigation of a Contactless Measuring Section in the Problem on High-Velocity Ballistic Flights

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Journal of Engineering Physics and Thermophysics Aims and scope

A method and system for contactless measurement of the velocity of flight of a thrown body over a measuring base in an air atmosphere and for the actuation of a recording apparatus by the signal formed as a result of the passage of the body through a measuring section are presented. The method proposed is based on the formation of normalized pulses of positive polarity for the synchronization of the activation of a recording apparatus by a definite coordinate of a body thrown. Results of calculation and experimental investigations of variable reluctance pickups in tests of high-velocity ballistic flights are presented. Relations allowing one to estimate the dependence of the magnetic induction in the core of a variable reluctance pickup on the value of the air gap between a magnet and the pickup are presented.

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References

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Correspondence to S. I. Gerasimov.

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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 94, No. 1, pp. 174–179, January–February, 2021.

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Gerasimov, S.I., Erofeev, V.I., Zubankov, A.V. et al. Mathematical Simulation and Experimental Investigation of a Contactless Measuring Section in the Problem on High-Velocity Ballistic Flights. J Eng Phys Thermophy 94, 165–170 (2021). https://doi.org/10.1007/s10891-021-02285-x

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  • DOI: https://doi.org/10.1007/s10891-021-02285-x

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