Encyclopaedia Index

TITLE : COLD FLOW NUMERICAL SIMULATION OF A TWO-DIMENSIONAL NOZZLELESS SOLID ROCKET MOTOR

BY : Aerospatiale - J F Chauvot DATE : 1992

DETAILS :

NOTES :

The pictures are as follows:
Experimental apparatus
Computational domain and close-up of the grid used for the turbulent computations.
Pressure distribution vs normalised axial distance.Both experimental and PHOENICS results are shown.
Axial velocity component vs normalised axial distance, on the symmetry axis.

DISCUSSION:

Full details of the PHOENICS simulation and the experimental results may be obtained in: CFD with PHOENICS at Aerospatiale, Espace & Defense An Overview J F Chauvot Presented at the 5th International PHOENICS User Conference, Nice, September 1992. Published in the International PHOENICS Journal Vol 6, No 3 1993.

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