Loading [MathJax]/jax/output/SVG/config.js
Prikladnaya Mekhanika i Tekhnicheskaya Fizika
RUS  ENG    JOURNALS   PEOPLE   ORGANISATIONS   CONFERENCES   SEMINARS   VIDEO LIBRARY   PACKAGE AMSBIB  
General information
Latest issue
Archive

Search papers
Search references

RSS
Latest issue
Current issues
Archive issues
What is RSS



Prikl. Mekh. Tekh. Fiz.:
Year:
Volume:
Issue:
Page:
Find






Personal entry:
Login:
Password:
Save password
Enter
Forgotten password?
Register


Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2010, Volume 51, Issue 5, Pages 5–16 (Mi pmtf1635)  

This article is cited in 5 scientific papers (total in 5 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
English version:
Journal of Applied Mechanics and Technical Physics, 2010, Volume 51, Issue 5, Pages 323–332
DOI: https://doi.org/10.1007/s10808-010-0080-4
Bibliographic databases:
Document Type: Article
UDC: 533.6.013.12: 533.6.011.5
Language: Russian
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
Citation in format AMSBIB
\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:
    1. 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  crossref
    2. 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  mathnet  crossref
    3. 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)  crossref
    4. Carmen Mihai, Alexandra Ene, Advances in Intelligent Systems and Computing, 954, Advances in Design for Inclusion, 2020, 457  crossref
    5. 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  crossref
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
    Statistics & downloads:
    Abstract page:62
    Full-text PDF :36
     
      Contact us:
     Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2025