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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2010, Volume 51, Issue 5, Pages 5–16
(Mi pmtf1635)
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This article is cited in 4 scientific papers (total in 4 papers)
Development of a parachute system for deceleration of flying vehicles in supersonic regimes
N. N. Pilyugina, V. S. Khlebnikovb a Institute of Mechanics at the Lomonosov, Moscow State University, Moscow, 119192, Russia
b Central Aerohydrodynamic Institute, Zhukovskii, 140180, Russia
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).
Keywords:
supersonic flow, Mach and Reynolds numbers, flow reconstruction, aerodynamic characteristics, load-parachute system, parachute.
Received: 23.09.2008 Accepted: 30.06.2009
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
Linking options:
https://www.mathnet.ru/eng/pmtf1635 https://www.mathnet.ru/eng/pmtf/v51/i5/p5
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