Numerical Modeling of Non-stationary Flow Near Lateral Surface of the Descent Module in the Martian Atmosphere for Wide Range of Attack Angles
Author:
Babakov Alexander V.ORCID
Publisher
Springer Singapore
Reference9 articles.
1. Holden, M.S., Wadhams, T.P., MacLean, M., Mundy, E., Parker, R.A.: Experimental studies in LENS I and X to evaluate real gas effects on hypervelocity vehicle performance. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007–204, pp. 1–17. American Institute of Aeronautics and Astronautics, Reno, Nevada, USA (2007) 2. Alexashkin, S.N., Martynov, M.B., Pichkhadze, K.M., Finchenko, V.S.: Results of integrated development tests of the Phobos-Grunt spacecraft’s descent module intended to deliver Phobos soil samples to earth. Sol. Syst. Res. 46(7), 502–510 (2012) 3. Golomazov, M.M., Finchenko, V.S.: Aerodynamic design of a vehicle in the Martian atmosphere under EXOMARS project. Sol. Syst. Res. 48(7), 541–548 (2014) 4. Finchenko, V.S., Ivankov, A.A., Shmatov, S.I., Mordvinkin, A.S.: Preliminary results of the calculated and experimental studies of the aerothermodynamic parameters of the EXOMARS landing module. Sol. Syst. Res. 49(7), 557–568 (2015) 5. Belotserkovskii, O.M., Severinov, L.I.: The conservative flow method and the calculation of the flow of a viscous heat-conducting gas past a body of finite size. Comput. Math. Math. Phys. 13(2), 141–156 (1973)
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