메뉴 건너뛰기




Volumn 10, Issue 4, 2006, Pages 295-308

Pulsatory phenomenon in a thrust optimized contour nozzle

Author keywords

Free shock separation; Restricted shock separation; Thrust optimized contour nozzle flow

Indexed keywords

FLOW OF FLUIDS; HYSTERESIS; NATURAL FREQUENCIES; OPTIMIZATION; PULSATILE FLOW;

EID: 33744808031     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.07.002     Document Type: Article
Times cited : (21)

References (17)
  • 1
    • 1442286940 scopus 로고    scopus 로고
    • Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle
    • Anh Thi N., Deniau H., Girard S., and Alziary de Roquefort T. Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle. Flow, Turbulence and Combustion 71 (2003) 161-181
    • (2003) Flow, Turbulence and Combustion , vol.71 , pp. 161-181
    • Anh Thi, N.1    Deniau, H.2    Girard, S.3    Alziary de Roquefort, T.4
  • 2
    • 0032101457 scopus 로고    scopus 로고
    • A new low-Reynolds-number nonlinear two-equation turbulence model for complex flows
    • Apsley D.D., and Leschziner M.A. A new low-Reynolds-number nonlinear two-equation turbulence model for complex flows. Int. J. Heat Fluid Flows 19 (1998) 209-222
    • (1998) Int. J. Heat Fluid Flows , vol.19 , pp. 209-222
    • Apsley, D.D.1    Leschziner, M.A.2
  • 3
    • 0028501729 scopus 로고
    • Numerical investigation of separated nozzle flows
    • Chen C.L., Chakravarthy S.R., and Hung C.M. Numerical investigation of separated nozzle flows. AIAA J. 32 9 (September 1994)
    • (1994) AIAA J. , vol.32 , Issue.9
    • Chen, C.L.1    Chakravarthy, S.R.2    Hung, C.M.3
  • 4
    • 33744818560 scopus 로고    scopus 로고
    • M. Frey, G. Hagemann, Status of flow separation prediction in rocket nozzles, AIAA Paper 98-3619, 1998
  • 5
    • 33744786883 scopus 로고    scopus 로고
    • M. Frey, G. Hagemann, Flow separation and side-loads in rocket nozzles, AIAA Paper 99-2815, 1999
  • 6
    • 49549162313 scopus 로고
    • The calculation of low-Reynolds number phenomena with a two-equation model of turbulence
    • Jones W.P., and Launder B.E. The calculation of low-Reynolds number phenomena with a two-equation model of turbulence. Int. J. Heat Mass Transfer 16 (1973) 1119-1130
    • (1973) Int. J. Heat Mass Transfer , vol.16 , pp. 1119-1130
    • Jones, W.P.1    Launder, B.E.2
  • 7
    • 0026140270 scopus 로고
    • Calculation of divergent channel flows with a multiple-time-scale turbulence model
    • Kim S.W. Calculation of divergent channel flows with a multiple-time-scale turbulence model. AIAA J. 29 4 (1991) 547-554
    • (1991) AIAA J. , vol.29 , Issue.4 , pp. 547-554
    • Kim, S.W.1
  • 8
    • 33744813885 scopus 로고    scopus 로고
    • R.W. MacCormack, Current status of numerical solutions of the Navier-Stokes equations, AIAA Paper 85-0032, 1985
  • 9
    • 0028486598 scopus 로고
    • Two-equation eddy-viscosity turbulence models for engineering applications
    • Menter F.R. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA J. 32 8 (1994)
    • (1994) AIAA J. , vol.32 , Issue.8
    • Menter, F.R.1
  • 10
    • 33744807826 scopus 로고    scopus 로고
    • L.H. Nave, G.A. Coffey, Sea levels side loads in high-area-ratio rocket engines, AIAA Paper 73-1284, 1973
  • 11
    • 33744809364 scopus 로고    scopus 로고
    • M. Onofri, F. Nasuti, The physical origins of side-loads in rocket nozzles, AIAA Paper 99-2587, 1999
  • 12
    • 33744786064 scopus 로고    scopus 로고
    • C. Pilinski, Étude numérique du décollement en tuyères supersoniques, Thèse de doctorat, University de Rouen, France, 2002
  • 14
    • 28644433499 scopus 로고    scopus 로고
    • Flow separation in a truncated ideal contour nozzle
    • Pilinski C., and Nebbache A. Flow separation in a truncated ideal contour nozzle. J. Turbulence 5 (2004) 014
    • (2004) J. Turbulence , vol.5 , pp. 014
    • Pilinski, C.1    Nebbache, A.2
  • 15
    • 33744807287 scopus 로고    scopus 로고
    • P. Reijasse, F. Bouvier, P. Servel, Experimental and numerical investigation of the Cap-Shock structure in overexpanded thrust-optimized nozzles, In: D.E. Zeitoun, J. Periaux, J.A. Désidéri, M. Marini (Eds.), West-East-High Speed Flow Field 2002, CIMNE, Barcelona, 2002
  • 16
    • 33744780544 scopus 로고    scopus 로고
    • J. Steger, R.F. Warming, Flux vector splitting of the inviscid gasdynamic equations with application to finite difference methods, NASA TM-78605, 1979
  • 17
    • 33744785206 scopus 로고    scopus 로고
    • M. Terhardt, G. Hagemann, M. Frey, Flow separation and side-load behavior of the vulcain engine, AIAA Paper 99-2762, 1999


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.