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Gas Flow in a Supersonic Nozzle with a Coaxially Arranged, Partially Permeable Cylindrical Insert

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REFERENCES

  1. Vinogradov, Yu.A., Ermolaev, I.K., and Leont'ev, A.I., Izv. Ross. Akad. Nauk Mekh. Zhidk. Gaza, 1999, no. 5, p. 205.

    Google Scholar 

  2. Abramovich, G.N., Prikladnaya gazovaya dinamika (Applied Gas Dynamics), Moscow: Nauka, 1953.

    Google Scholar 

  3. Kutateladze, S.S. and Leont'ev, A.I., Teplomassoobmen i trenie v turbulentnom pogranichnom sloe (Heat and Mass Transfer and Friction in a Turbulent Boundary Layer), Moscow: Energoatomizdat, 1985.

    Google Scholar 

  4. Gazodinamicheskaya temperaturnaya stratifikatsiya (Otchet) (Gasdynamic Temperature Stratification: A Report), Moscow: NII Mekhaniki Mosk. Gos. Univ. (Research Inst. of Mechanics, Moscow State Univ.), 2000, no. 4572, p. 22.

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Vinogradov, Y.A., Ermolaev, I.K. & Leont'ev, A.I. Gas Flow in a Supersonic Nozzle with a Coaxially Arranged, Partially Permeable Cylindrical Insert. High Temperature 38, 969–971 (2000). https://doi.org/10.1023/A:1004109911164

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  • DOI: https://doi.org/10.1023/A:1004109911164

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