Numerical investigation of transient nozzle flow

Shock Waves

Volumn 12, Issue 5, 2003, Pages 403-411

  Mouronval, A S ^a   Hadjadj, A ^a   Kudryavtsev, A N ^b   Vandromme, D ^a  

^a University of Rouen Normandy   (France)

^b KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

Author keywords

Nozzle flow; Numerical simulation; Shock wave; Starting process

Indexed keywords

EID: 0037353130     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00193-002-0171-0     Document Type: Article

References (21)

1. Amann HO (1969) Experimental study of the starting process in a reflection nozzle. Phys. Fluids Supplement 12:150-153
2. Blin L (1999) Modélisation statistique et simulation des grandes échelles des écoulements turbulents. Application aux inverseurs de poussée. Ph. D. thesis, University of Rouen, France
3. Blin L, Hadjadj A, Vervisch L (1999) Large Eddy Simulation of Compressible Turbulent Flows. AIAA-Paper 99-0787, 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV
4. Chen CL, Chakravarthy SL, Hung CM (1994) Numerical Investigation of Separated Nozzle Flows. AIAA Journal 32:1836-1843
5. Courant R, Friedrichs KO (1991) Supersonic flow and shock waves. Applied Mathematical Sciences. Springer-Verlag
6. Harten A, Engquist B, Osher S, Chakravarty S (1987) Uniform high order essentially non oscillatory schemes III. J. Comput. Phys. 71:231-301
7. Igra O, Wang L, Falcovitz J, Amann HO (1998) Simulation of the starting flow in a wedge-like nozzle. Shock Waves 8:235-242
8. Jacobs PA (1991) Simulation of transient flow in a shock tunnel and a high Mach number nozzle. NASA CR 187606
9. Jiang G, Shu CW (1996) Efficient implementation of weighted essentially non-oscillatory schemes. J. Comput. Phys. 126:202-228
10. Kudryavtsev AN, Khotyanovsky DV (1998) A numerical method for simulation of unsteady phenomena in high speed shear flows. ICMAR'98, Int. Conf. on Methods of Aerophysical Research, Novosibirsk
11. Kudryavtsev A, Hadjadj A (2001) Visualisation graphique en mécanique des fluides numérique. In the proceedings of Fluvisu 2001 conference, 18-21 June 2001, Rouen, France
12. Liu XD, Osher S, Chan T (1994) Weighted essentially non oscillatory schemes. J. Comput. Phys. 115:200-212
13. Nasuti F, Onofri M (1994) Transient Flow analysis of nozzle start-up by a shock fitting technique. Unsteady Flows in Aeropropulsion, edited by W. Ng. D. Fant and L. Povinelli, AD-40:127-135, ASME, New York, pp. 127-135
14. Nasuti F, Onofri M (1998) Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles. AIAA Journal 36:809-815
15. Ostlund J, Damgaard M, Frey M (2001) Side-load phenomena in highly over-expanded rocket nozzles. AIAA Paper 2001-3684
16. Prodromou P, Hillier R (1992) Computation of unsteady nozzle flows. Proc. of the 18th ISSW Sendai, Japan, II:1113-1118
17. Saito T, Timofeev EV, Sun M, Takayama K (1999) Numerical and experimental study of 2-D nozzle starting process. Paper 4090, in the Proceedings of the 22nd ISSW, Imperial College, London, UK, July 18-23
18. Shu CW, Osher S (1989) Efficient implementation of essentially non-oscillatory shock capturing schemes. J. Comput. Phys. 83:32-78
19. Smith CE (1964) An analytic study of the starting process in a hypersonic nozzle. Proc. Heat Transfer and Fluid Mech. Institute, p. 198, Stanford Univ. Press
20. Smith CE (1966) The starting process in a hypersonic nozzle. J. Fluid Mech. 24:625-640
21. Tokarcik-Polsky S, Cambier JL (1994) Numerical study of transient flow phenomena in shock tunnels. AIAA Journal 32:971-978