Abstract
In order to clarify the results of experimental studies with free-spinning aircraft models in a vertical wind tunnel, the analysis of the force pitching moment coefficients acting on the model, full-scale aircraft and their elements was carried out. It is shown that some differences in these coefficients are acceptable, which is confirmed by a satisfactory convergence of the results of model studies and full-scale aircraft flight tests.
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 79 - 86.
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Golovkin, M.A., Efremov, A.A., Kritskii, B.S. et al. To the Estimation of Force and Pitching Moment Coefficients Acting on the Model, Full-Scale Aircraft and Their Elements at Supercritical Angles of Attack and in a Spin. Russ. Aeronaut. 63, 643–651 (2020). https://doi.org/10.3103/S106879982004011X
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DOI: https://doi.org/10.3103/S106879982004011X