Processing math: 100%
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, 2014, Volume 55, Issue 5, Pages 165–171 (Mi pmtf1036)  
This article is cited in 4 scientific papers (total in 4 papers)

Damping characteristics of a reentry vehicle at hypersonic velocities

N. P. Adamova, L. N. Puzyreva, A. M. Kharitonova, E. A. Chasovnikova, A. A. Dyadkinb, A. N. Krylovb

a Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia
b Korolev Rocket and Space Corporation Energia, Korolev, 141071, Russia
Full-text PDF (542 kB) Citations (4)
Abstract: The experimental equipment, model, test conditions, and methods used for determining the streamwise damping on a setup with free oscillations on rolling bearings are described. Characteristics of aerodynamic damping of the model with two positions of the rotation axis and Mach numbers M=2,4 and 6 are measured. Irregular oscillations of the model with a greater displacement of the rotation axis with respect to the longitudinal axis are found to arise at M=2.
Keywords: reentry vehicle model, free oscillations, frequency of oscillations, damping decrement, longitudinal damping.
Received: 12.03.2013
Revised: 17.10.2013
English version:
Journal of Applied Mechanics and Technical Physics, 2014, Volume 55, Issue 5, Pages 870–876
DOI: https://doi.org/10.1134/S0021894414050162
Bibliographic databases:
Document Type: Article
UDC: 533.6.011.55
Language: Russian
Citation: N. P. Adamov, L. N. Puzyrev, A. M. Kharitonov, E. A. Chasovnikov, A. A. Dyadkin, A. N. Krylov, “Damping characteristics of a reentry vehicle at hypersonic velocities”, Prikl. Mekh. Tekh. Fiz., 55:5 (2014), 165–171; J. Appl. Mech. Tech. Phys., 55:5 (2014), 870–876
Citation in format AMSBIB
\Bibitem{AdaPuzKha14}
\by N.~P.~Adamov, L.~N.~Puzyrev, A.~M.~Kharitonov, E.~A.~Chasovnikov, A.~A.~Dyadkin, A.~N.~Krylov
\paper Damping characteristics of a reentry vehicle at hypersonic velocities
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2014
\vol 55
\issue 5
\pages 165--171
\mathnet{http://mi.mathnet.ru/pmtf1036}
\elib{https://elibrary.ru/item.asp?id=22318139}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2014
\vol 55
\issue 5
\pages 870--876
\crossref{https://doi.org/10.1134/S0021894414050162}
Linking options:
  • https://www.mathnet.ru/eng/pmtf1036
  • https://www.mathnet.ru/eng/pmtf/v55/i5/p165
    • This publication is cited in the following 4 articles:
    1. N. P. Adamov, A. M. Kharitonov, E. A. Chasovnikov, A. A. Dyadkin, A. N. Krylov, “Methodical research of unsteady aerodynamic characteristics of the main-stage separation unit of emergency rescue system at supersonic speeds”, Thermophys. Aeromech., 28:1 (2021), 1  crossref
    2. N. P. Adamov, A. M. Gurin, E. A. Chasovnikov, AIP Conference Proceedings, 2027, 2018, 030151  crossref
    3. N. P. Adamov, A. M. Kharitonov, E. A. Chasovnikov, A. A. Dyad'kin, A. N. Krylov, E. N. Aleksandrov, “Experimental study of aerodynamic characteristics of a reentry vehicle on a setup with free oscillations at supersonic velocities”, Thermophys. Aeromech., 23:6 (2016), 791  crossref
    4. N. P. Adamov, A. M. Kharitonov, E. A. Chasovnikov, A. A. Dyad'kin, M. I. Kazakov, A. N. Krylov, A. Yu. Skorovarov, “Aerodynamic characteristics of reentry vehicles at supersonic velocities”, Thermophys. Aeromech., 22:5 (2015), 535  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:53
    Full-text PDF :23
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2025