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, 2000, Volume 41, Issue 5, Pages 171–179 (Mi pmtf2991)  
This article is cited in 14 scientific papers (total in 14 papers)

Numerical analysis of the effect of local energy supply on the aerodynamic drag and heat transfer of a spherically blunted body in a supersonic air flow

V. A. Levina, V. G. Gromovb, N. E. Afoninab

a Institute of Automation and Control Processes, Far-Easter Division, Russian Academy of Sciences, 690041, Vladivostok
b Institute of Mechanics of Moscow State University, 117192, Moscow
Full-text PDF (310 kB) Citations (14)
Abstract: The effect of local source of energy in a supersonic flow on the aerodynamic drag and heat transfer of a spherically blunted body is studied numerically. Calculations are performed on the basis of the Navier-Stokes equations for a thermally equilibrium model of air. Data on the effect of the intensity and size of the energy source on the wave drag, friction, and heat transfer are obtained. Particular attention is given to studying the effect of drag reduction by means of a focused heat source. The gas-dynamic nature of this effect is studied. The limits of drag reduction are estimated, and optimal conditions of heat supply are determined.
Received: 10.03.2000
English version:
Journal of Applied Mechanics and Technical Physics, 2000, Volume 41, Issue 5, Pages 915–922
DOI: https://doi.org/10.1007/BF02468738
Bibliographic databases:
Document Type: Article
UDC: 534.222.2
Language: Russian
Citation: V. A. Levin, V. G. Gromov, N. E. Afonina, “Numerical analysis of the effect of local energy supply on the aerodynamic drag and heat transfer of a spherically blunted body in a supersonic air flow”, Prikl. Mekh. Tekh. Fiz., 41:5 (2000), 171–179; J. Appl. Mech. Tech. Phys., 41:5 (2000), 915–922
Citation in format AMSBIB
\Bibitem{LevGroAfo00}
\by V.~A.~Levin, V.~G.~Gromov, N.~E.~Afonina
\paper Numerical analysis of the effect of local energy supply on the aerodynamic drag and heat transfer of a spherically blunted body in a supersonic air flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2000
\vol 41
\issue 5
\pages 171--179
\mathnet{http://mi.mathnet.ru/pmtf2991}
\elib{https://elibrary.ru/item.asp?id=17261946}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2000
\vol 41
\issue 5
\pages 915--922
\crossref{https://doi.org/10.1007/BF02468738}
Linking options:
  • https://www.mathnet.ru/eng/pmtf2991
  • https://www.mathnet.ru/eng/pmtf/v41/i5/p171
    • This publication is cited in the following 14 articles:
    1. V. I. Lysenko, A. V. Starov, “Experimental study on combustion within a supersonic boundary layer and its effect on laminar-turbulent transition”, Thermophys. Aeromech., 30:2 (2023), 263  crossref
    2. Ya. V. Khankhasaeva, “Energy input influence on aerodynamic characteristics and heat flux occuring at 3D supersonic flow past a model aircraft”, Math. Models Comput. Simul., 15:4 (2023), 765–779  mathnet  crossref  crossref  mathscinet
    3. V. I. Lysenko, S. A. Gaponov, B. V. Smorodsky, A. N. Semenov, S. O. Morozov, A. V. Starov, “Influence of distributed hydrogen injection and combustion on supersonic boundary layer stability and transition”, Physics of Fluids, 35:9 (2023)  crossref
    4. D. I. Zaripov, V. A. Ivashchenko, S. A. Panteleev, A. A. Luk'yanov, R. I. Mullyadzhanov, “Direct Numerical Simulation of the Turbulent Flow Laminarization in a Pipe at Re = 5000”, Russ. Aeronaut., 66:4 (2023), 723  crossref
    5. S. A. Gaponov, “Stability of Supersonic Boundary Layer with Internal Heat Supply and Injection of Homogeneous Gas through a Porous Wall”, jour, 18:2 (2023), 54  crossref
    6. Shagufta Rashid, Fahad Nawaz, Adnan Maqsood, Shuaib Salamat, Rizwan Riaz, “Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 236:14 (2022), 2851  crossref
    7. N.A. Brykov, V.N. Emelyanov, A.G. Karpenko, K.N. Volkov, “Flows of real gas in nozzles with unsteady local energy supply”, Computers & Mathematics with Applications, 81 (2021), 702  crossref
    8. S. A. Gaponov, “Stability of a supersonic boundary layer with heat supply to a narrow band of the layer”, Thermophys. Aeromech., 28:3 (2021), 327  crossref
    9. M. Ashwin Ganesh, Bibin John, “Concentrated energy addition for active drag reduction in hypersonic flow regime”, Acta Astronautica, 142 (2018), 221  crossref
    10. I. Yu. Kudryashov, A. E. Lutsky, Ya. V. Khankhasaeva, “Numerical simulation of the energy deposition influence on the base flow”, Math. Models Comput. Simul., 8:2 (2016), 207–218  mathnet  mathnet  crossref  scopus
    11. John Bibin, Kulkarni Vinayak, “Investigation of Energy Deposition Technique for Drag Reduction at Hypersonic Speeds”, AMM, 367 (2013), 222  crossref
    12. Hong Yan, Xiao Jing Yu, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013  crossref
    13. Xiaojing Yu, Hong Yan, “Parametric Study of Laser Energy Deposition in Mach 8 Bow Shock”, International Journal of Flow Control, 4:1-2 (2012), 19  crossref
    14. S. M. Aulchenko, V. P. Zamuraev, A. P. Kalinina, “Controlling a transonic flow around airfoils by means of energy supply with allowance for real properties of air”, J. Appl. Mech. Tech. Phys., 51:3 (2010), 332–337  mathnet  mathnet  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:68
    Full-text PDF :28
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2025