Abstract
The domain of the parameters in which the aerodynamic drag of hypersonic pyramidal bodies, whose wave component is calculated within the framework of conical flows with the boundary layer displacement thickness taken into account, agrees satisfactorily with the experimental data is found. The calculation model is also applicable in the region of minimum aerodynamic drag of star-shaped bodies in the class of conical bodies equivalent in length and mid-sectional area.
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References
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Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 5, pp. 69–79, September–October, 1996.
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Zubin, M.A., Ostapenko, N.A. & Chulkov, A.A. Simulation of the aerodynamic drag of three-dimensional star-shaped bodies at hypersonic velocities. Fluid Dyn 31, 686–693 (1996). https://doi.org/10.1007/BF02078220
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DOI: https://doi.org/10.1007/BF02078220