On the Compressible Hart-McClure Mean Flow Motion in Simulated Rocket Motors

Abstract

, a closed-form representation of the compressible correction. In view of the favorable convergence properties of the Rayleigh- Janzen expansion, the resulting approximation can be relied upon from the headwall down to the sonic point and slightly beyond in a long porous tube or nozzleless chamber. Based on the simple closed-form expressions that prescribe this motion, the principal flow attributes are quantified parametrically and compared to existing incompressible and one-dimensional theories. In this effort, the local Mach number and pressure are calculated and shown to provide an improved formulation when gauged against one-dimensional theory. Our results are also compared to the two-dimensional axisymmetric solution obtained by Majdalani (Majdalani, J., On Steady Rotational High Speed Flows: The Compressible Taylor-Culick Profile, Proceedings of the Royal Society of London, Series A, Vol. 463, No. 2077, 2007, pp. 131-162). After rescaling the axial coordinate by the critical length Ls, a parametrically-free form is obtained that is essentially independent of the Mach number. This behavior is verified analytically, thus confirming Majdalani's universal similarity with respect to the critical distance. A secondary verification by computational fluid dynamics is also undertaken. When compared to existing rotational models, the compressible Hart-McClure plug-flow requires, as it should, a slightly longer distance to reach the speed of sound at the centerline. At that point, however, the entire cross-section is fully choked.