Experimental investigation of combustion stabilization in supersonic flow using free recirculating zone

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 93-103

  Sabel'nikov V A ^a   Korontsvit, Yu Ph ^a   Ivanyushkin, A K ^a   Ivanov, V V ^a  

^a CENTRAL AEROHYDRODYNAMIC INSTITUTE TSAGI   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC PRESSURE; COMBUSTION; SHOCK WAVES; STABILIZATION; SUPERSONIC FLOW;

EXPERIMENTAL INVESTIGATIONS; GAS LIQUIDS; INITIAL THICKNESS; NORMAL SHOCK WAVES; SELF IGNITION; SUPERSONIC JETS; TOTAL TEMPERATURES; TWO DIMENSIONAL CHANNELS;

SUPERSONIC AERODYNAMICS;

EID: 84983156910     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1515     Document Type: Conference Paper

References (17)

1. Zatoloka, V.V., Ivanyushkin, A.K. and Nikolaev, A.V. Interference of concentrated vortices with shock wave in inlet. Breakup of vortices. Uchenye Zapiski TsAGI, 6, No. 2, pp. 134-138, 1975 (In Russian).
2. Zatoloka, V.V., Ivanyushkin, A.K. and Nikolaev A.V. Interference of vortexes with shocks in airscoops. Dissipation of vortexes. Fluid Mechanics - Soviet Research, 7, No. 4, July - August, pp. 153-158, 1978.
3. Ivanyushkin, A.K., Korotkov, Yu.V. and Nikolaev, A.V. Some peculiarities of interference of shock waves with aerodynamic wake behind body. Uchenye Zapiski TsAGI, 10, No. 5, pp. 33-42, 1989 (In Russian).
4. Delery, J., Horovitz, E., Leuchter, O. and Solingac, J. Studes foundamentals sar les e'coulements tourbillonares. La Recherche Aerospatiale, No.2, pp.81-104, 1984.
5. Mettwally, O., Settles, G., Horsman C. An Experimental Study of Shock Wave/Vortex Interaction. AIAA Paper 89-0082, 12 p., 1989.
6. Glotov, G.Ph. Interference of concentrated vortex with shock waves in free flow and nondesigned jets. Uchenye Zapiski TsAGI, 10, No. 5, pp. 21-32, 1989 (In Russian).
7. Michael, K., Smart, K.M., and Kalkhoran, I. M. Effect of Shock Strength on Oblique Shock-Wave/Vortex Interaction. AIAA Journal, 33, No. 11, pp. 2137-2143, 1995.
8. Kalkhoran, I.M., Smart, K.M. and Betti, A. Interaction of supersonic wing-tip vortices with a normal shock. AIAA Journal, 34, No.9, pp. 1855-1861, 1996.
9. Winterfeld, G. On the burning limits of flameholderstabilized flames in supersonic flow. AGARD, IX, 2, No. 34, p. 12, 1968.
10. Sabel'nikov, V.A. Supersonic turbulent combustion of nonpremixed gases - status and perspectives. In: Advanced Computation & Analysis of Combustion. Moscow ENAS Publishers, pp. 208-237, 1997.
11. Figueira da Silva, L.F., Sabelnikov, V.A., and Deshaies, B. The stabilization of supersonic combustion by a free recirculating bubble: a numerical study. AIAA Journal, 35, No. 11, pp. 1782-1784, 1997.
12. Shchetinkov, E.S. Physics of gas combustion. Nauka, Moscow, 1965 (In Russian)
13. Zakkay, V. and Sinha, R. Residence time within a wake recirculation region in an axisymmetric supersonic flow. AIAA Paper 70-111, 11 p., 1970.
14. Baev, V.K., Golovichev, V.I., Tret'yakov, P.K. et al. Combustion in supersonic flow. Nauka, Moskow, Novosibirsk, 1984 (In Russian)
15. Westbrook, K., and Dryer, F.L. Chemical kinetic modeling of hydrocarbon combustion. Progress in Energy and Combustion Science, 10, pp.1-57, 1984.
16. Avrashkov, V.N., Baranovsky, S.I. and Levin, V.M. Gasdynamic features of supersonic kerosene combustion in model combustion chamber. AIAA Paper 90-5268, 7 p., 1990.
17. Ivanyushkin, A.K. and Korotkov, Yu.V. Influence of flow vorticity on diffuser start at supersonic and hypersonic speeds." TsAGI Workshop - School "Fluid Mechanics": Research in Hypersonic Flows and Hypersonic Technologies. TsAGI, pp. 27-28, 1994.