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A delta wing with blunt edges at low angles of attack in hypersonic flow

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References

  1. V. V. Lunev, “Hypersonic flow past a triangular flat plate with blunt leading edges”, Izv. AN SSSR, Mekhanika, no. 3, 1965.

  2. A. V. Krasil'nikov, “Effect of Mach number on hypersonic flow past a delta wing with blunt leading edges”, Izv. AN SSSR, MZhF [Fluid Dynamics], no. 1, 1967.

  3. G. G. Chernyi, Gas Flow at High Supersonic Speeds [in Russian], Fizmatgiz, Moscow, 1959.

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  4. V. I. Kholyavko, “Hypersonic gas flow past a flat blunt plate at low angles of attack”, Izv. AN SSSR, OTN, no. 2, 1964.

  5. H. S. Tsien, “The Poincare—Lighthill—Kuo method”, Advances in Appl. Mech., Acad. Press Inc., N. Y., vol. 4, 1956.

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Authors and Affiliations

  1. Moscow

    A. V. Krasil'nikov

Authors
  1. A. V. Krasil'nikov
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Additional information

In conclusion the author wishes to thank V. V. Lunev for evaluating the results.

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Krasil'nikov, A.V. A delta wing with blunt edges at low angles of attack in hypersonic flow. Fluid Dyn 3, 101–104 (1968). https://doi.org/10.1007/BF01029548

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  • DOI: https://doi.org/10.1007/BF01029548

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