Abstract
The effect of heating on the mass of load-carrying structures is analyzed using the weight Komarov formula in the framework of the design calculations by examples of a panel and spar. The results obtained have been compared with the data on real structures of supersonic passenger aircraft and aerospace aircraft of reusable transport systems.
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Original Russian Text © Z.J. Wang, L.H. Kang, S. Huang, and A.S. Kretov, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 1, pp. 36–42.
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Wang, Z.J., Kang, L.H., Huang, S. et al. Effect of heating on the load-carrying structure mass. Russ. Aeronaut. 57, 45–54 (2014). https://doi.org/10.3103/S1068799814010073
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DOI: https://doi.org/10.3103/S1068799814010073