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Flow of a subsonic or transsonic stream around the afterbody of bodies of rotation

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Literature Cited

  1. H. McDonald and P. F. Hughes, “Correlation of high subsonic afterbody drag in the presence of a propulsive jet or support sting,” J. Aircraft,2, No. 3, 202–207 (1965).

    Google Scholar 

  2. R. S. Armstrong and S. R. Miller, “Subsonic aerodynamic performance of nozzle installations in supersonic airplanes,” J. Aircraft,5, No. 3 (1968).

  3. D. Bergman, “Effects of engine exhaust flow on boattail drag,” AIAA paper No. 132 (1970).

  4. M. Ya. Ivanov, “One variational problem in supersonic gas dynamics,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 1, 97–100 (1968).

    Google Scholar 

  5. J. R. Spreiter and A. Y. Alksne, “Slender-body theory based on approximate solution of the transonic flow equation,” NASA TR, R-2 (1965).

  6. W. Presz, M. Konarski, and E. Grund, “Prediction of installed nozzle flow fields,” AIAA Paper No. 700 (1970).

  7. W. Frossel, “Experimentelle Untersuchung der Kompressiblen Strömung an und in der Nähe einer gewölbten Wand,” Mitt. Max Planck Inst. Strömungsforschung, No. 4105, Göttingen (1951).

  8. G. L. Grodzovskii, A. A. Nikol'skii, G. P. Svishchev, and G. I. Taganov, Supersonic Flows of Gas in Perforated Boundaries [in Russian], Izd. Mashinostroenie, Moscow (1967).

    Google Scholar 

  9. Yu. B. Lifshits, “Calculation of transsonic flow around a symmetrical profile in a free jet,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 1 (1969).

  10. R. Magnus and H. Yoshihara, “Inviscidtranssonic flow over airfoils,” AIAA Paper No. 48 (1970).

  11. Yu. M. Lipnitskii and Yu. B. Lifshits, “Calculation of the flow of a transsonic stream around bodies of rotation,” Prikl. Mat. i Mekhan.,34, No. 3 (1970).

  12. S. K. Godunov, “Difference method for the numerical calculation of breakaway solutions of the equations of hydrodynamics,” Matem. Sb.,47(89) No. 3, 271–306 (1959).

    Google Scholar 

  13. A. N. Kraiko and M. Ya. Ivanov, “Numerical solution of the direct problem of mixed flow in nozzles,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 5, 77–83 (1969).

    Google Scholar 

  14. S. K. Godunov, A. V. Zabrodin, and G. P. Prokonov, “Difference scheme for two-dimensional unsteadystate problems of gas dynamics, and calculation of flow with a departing shock wave,” Zh. Vyshislit. Mat. i Mat. Fiz.,1, No. 6, 1020–1050 (1961).

    Google Scholar 

  15. G. M. Bam-Zelikovich, “Calculation of the breakaway of a boundary layer,” Izv. Akad. Nauk SSSR, Otd. Tekh. Nauk, No. 12 (1954).

  16. M. Pinzola and C. F. Lo, “Boundary interference at subsonic speeds in wind tunnels with ventilated walls,” AEDC-TR-69-47, 115 (1969).

  17. V. S. Avduevskii, “Method for calculating a three-dimensional boundary layer in a compressible gas,” Izv. Akad. Nauk SSSR, Otd. Tekh. Nauk, No. 4 (1962).

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Moscow. Translated from Izvestiya Akademii Nauk SSSR. Mekhanika Zhidkosti i Gaza, No. 6, pp. 162–168, November–December, 1972.

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Tagirov, R.K. Flow of a subsonic or transsonic stream around the afterbody of bodies of rotation. Fluid Dyn 7, 1013–1018 (1972). https://doi.org/10.1007/BF01176124

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  • DOI: https://doi.org/10.1007/BF01176124

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