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Influence of the unit Reynolds number on transition in a supersonic boundary layer

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Literature cited

  1. A. Henderson, “Hypersonic viscous flows,∝ in: Current Problems of Gas dynamics,∝ [Russian translation], Mir, Moscow (1971).

    Google Scholar 

  2. V. Ya. Borova, “The influence of the unit Reynolds number on measurements of the aerodynamic and thermal characteristics of bodies in wind tunnels,∝ Trudy Tsentral'nogo Aérogidrodinamicheskogo Instituta, Issue 1374, No. 5 (1972).

  3. V. V. Struminskii, A. M. Kharitonov, and V. V. Chernykh, “Experimental study of the transition of a laminar boundary layer into a turbulent one at supersonic velocities,∝ Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 2 (1972).

  4. S. R. Pate and C. J. Schueler, “Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels,∝ AIAA J.7, No. 3 (1969).

  5. V. I. Kornilov, V. Ya. Levchenko, and A. M. Kharitonov, “Study of boundary-layer transition on wing profile at supersonic velocities,∝ Izv. Sibirsk. Otd. Akad. Nauk SSSR, Ser. Tekh. Nauk,1, No. 3 (1971).

  6. R. Michel and V. Schmitt, “Résultats sur la region de transition de la couche limite en hypersonique,∝ Aéronaut. et Astronaut., No. 19 (1970).

  7. J. L. Potter, “Observations on the influence of ambient pressure on boundary-layer transition,∝ AIAA J.,6, No. 10 (1968).

  8. J. L. Potter and J. D. Whitefield, “Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flows,∝ J. Fluid. Mech.,12, pt. 4 (1962).

  9. G. I. Bagaev, V. A. Lebiga, V. G. Pridanov, and V. V. Chernykh, The T-325 ultrasonic wind tunnel with a lower turbulence. Aerophysical studies [in Russian], In-t Teoret. Prikl. Mekhano, SO AN SSSR, Novosibirsk (1972).

    Google Scholar 

  10. E. Reshotko, “Stability theory as a guide to the evaluation of transition data,∝ AIAA J.7, No. 6 (1969).

  11. G. I. Taylor, “Statistical theory of turbulence, V. Effect of turbulence on boundary layer,∝ Proc. Roy. Soc., Ser. A,156 (1936).

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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 150–153, July–August, 1974.

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Kharitonov, A.M., Chernykh, V.V. Influence of the unit Reynolds number on transition in a supersonic boundary layer. Fluid Dyn 9, 625–628 (1974). https://doi.org/10.1007/BF01031324

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