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Experimental investigation of a hypersonic flow around an oscillating flared body

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Literature cited

  1. D. B. Kirk and G. T. Chapmen, “Free-flight tests of a blunt-nosecf flare-stabilized body at speeds to 8.2 km/sec,” J. Spac. and Rockets,3, No. 3, 374–378 (1966).

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  3. S. M. Belotserkovskii, B. K. Skripach, and V. Tabachnikov, “Determining the coefficients of rotating derivatives in aerodynamic tubes,” Izv. Akad Nauk SSSR, Mekhan. i Mashinostr., No. 3 (1964).

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Authors and Affiliations

  1. Moscow

    V. I. Lagutin, D. G. Levchuk & V. N. Shmanenkov

Authors
  1. V. I. Lagutin
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  2. D. G. Levchuk
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  3. V. N. Shmanenkov
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 189–191, September-October, 1970.

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Lagutin, V.I., Levchuk, D.G. & Shmanenkov, V.N. Experimental investigation of a hypersonic flow around an oscillating flared body. Fluid Dyn 5, 882–885 (1970). https://doi.org/10.1007/BF01017313

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  • DOI: https://doi.org/10.1007/BF01017313

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