Hypersonic flow over bodies in tandem and its relevance to ballute design
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A computational study of hypersonic flow over two bodies in tandem shows that if the second body is simply connected, the flow is violently unsteady in a similar way as in spiked body flow. The worst part of the unsteadiness can be avoided by making the second body in the shape of a ring. If this arrangement is used for aerocapture of a spacecraft, the ring requires significantly less gas than the simply connected body for the same drag. The ring could be given radial lift to counteract radial tether force.
[1] D. J. Maull,et al. Hypersonic flow over axially symmetric spiked bodies , 1960, Journal of Fluid Mechanics.
[2] J. J. Quirk,et al. AMRITA: A computational facility (for CFD modelling) , 1998 .
[3] Hans G. Hornung. Oblique shock reflection from an axis of symmetry , 2000, Journal of Fluid Mechanics.
[4] A. Rasheed,et al. Experimental investigation of the flow over a toroidal aerocapture ballute , 2001 .