Abstract:
Aerodynamic problems arising during design and development of braking systems for re-entry vehicles are analyzed. Aerodynamic phenomena and laws valid in a supersonic flow around a pair of bodies having different shapes are studied. Results of this research can be used in solving application problems (arrangement and optimization of experiments; design and development of various braking systems for re-entry vehicles moving with supersonic speeds in the atmosphere).
Citation:
N. N. Pilyugin, V. S. Khlebnikov, “Development of a parachute system for deceleration of flying vehicles in supersonic regimes”, Prikl. Mekh. Tekh. Fiz., 51:5 (2010), 5–16; J. Appl. Mech. Tech. Phys., 51:5 (2010), 323–332
\Bibitem{PilKhl10}
\by N.~N.~Pilyugin, V.~S.~Khlebnikov
\paper Development of a parachute system for deceleration of flying vehicles in supersonic regimes
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2010
\vol 51
\issue 5
\pages 5--16
\mathnet{http://mi.mathnet.ru/pmtf1635}
\elib{https://elibrary.ru/item.asp?id=15234914}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2010
\vol 51
\issue 5
\pages 323--332
\crossref{https://doi.org/10.1007/s10808-010-0080-4}
Linking options:
https://www.mathnet.ru/eng/pmtf1635
https://www.mathnet.ru/eng/pmtf/v51/i5/p5
This publication is cited in the following 5 articles:
A. V. Babakov, “Numerical Study of the Flow near a Descent Vehicle with the Parachute System's Canopies in Its Near Wake in Supersonic Motion”, Math Models Comput Simul, 17:1 (2025), 1
A. V. Babakov, “Chislennoe izuchenie techeniya okolo spuskaemogo apparata s kupolami parashyutnoi sistemy v ego blizhnem slede pri sverkhzvukovom dvizhenii”, Matem. modelirovanie, 36:5 (2024), 3–18
Jianhui Fan, Jiaao Hao, Chih-Yung Wen, Xiaopeng Xue, “Unsteady Supersonic Flows Past Two-Body Configurations with Different Separation Distances”, J. Aerosp. Eng., 36:1 (2023)
Carmen Mihai, Alexandra Ene, Advances in Intelligent Systems and Computing, 954, Advances in Design for Inclusion, 2020, 457
Koichi MORI, Kazuma KUZUO, “Canopy Shape Effects on Oscillation of Supersonic Parachute at Mach 3”, AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 17 (2018), 255