Role of Wall Shape on the Transition in Dual-Bell Nozzles
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[1] G. Rao. Exhaust Nozzle Contour for Optimum Thrust , 1958 .
[2] D. Migdal,et al. Truncated Perfect Nozzles in Optimum Nozzle Design , 1961 .
[3] M. Horn,et al. Dual-bell altitude compensating nozzles , 1993 .
[4] Francesco Nasuti,et al. Analysis of unsteady supersonic viscous flows by a shock-fitting technique , 1996 .
[5] Gerald Hagemann,et al. A critical assessment of dual-bell nozzles , 1997 .
[6] E. Reske,et al. Evaluation of altitude compensating nozzle concepts for RLV , 1997 .
[7] G. Dumnov,et al. Dual bell nozzles for rocket engines of launch vehicle upper stages and orbitral transfer vehicles , 1997 .
[8] Gerald Hagemann,et al. Advanced Rocket Nozzles. , 1998 .
[9] F. Nasuti,et al. Flow analysis and methods of design for dual-bell nozzles , 2001 .
[10] E. Martelli,et al. Numerical Study of Transition Between the Two Operating Modes of Dual-Bell Nozzles , 2002 .
[11] Gerald Hagemann,et al. Experimental and analytical design verification of the dual-bell concept , 2000 .
[12] F. Nasuti. A Multi-Block Shock-Fitting Technique to Solve Steady and Unsteady Compressible Flows , 2003 .
[13] Renato Paciorri,et al. Compressibility Correction for the Spalart-Allmaras Model in Free-Shear Flows , 2003 .