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Abstract content <br> (Max 300 words)<br><a href="http://events.saip.org.za/getFile.py/access?resId=0&materialId=0&confId=34" target="_blank">Formatting &<br>Special chars</a>
Theoretical work on transforming the Navier-Stokes equations into arbitrarily accelerating frames has included the continuity, momentum, and energy conservation equations [2] [3]. An analysis of the momentum equation in non-dimensional terms leads to an acceleration parameter that appears to be new in fluid physics, but is known in cosmology.
A selection of cases for rectilinear acceleration has been chosen [4][5] to illustrate the point that this parameter alone does not govern regimes of flow about significantly accelerating bodies, and reference must be made, above all, to the Mach number for transonic effects. Other parameters from the literature on impulsive start-up in wind tunnels are also shown to be useful in delimiting regimes of flow, such as the Freymuth start-up time [1]. Two dominant effects in fluid dynamics with accelerating objects are shown to be flow history, a term being used to cover the difference between an instantaneous flow field with an accelerating body and the flow field about the same body at steady state, and the dependence of stagnation pressure on acceleration. The dependence of these effects on the proposed dimensionless parameters is explored.
[1] P. Freymuth, W. Bank, and M. Palmer. Z. Flugwiss. Weltraumforsch 7:392–400, 1983.
[2] I.M.A. Gledhill, K. Forsberg, P. Eliasson, J. Baloyi, and J. Nordström. Aerospace Science and Technology , 13(4):197–203, 2009.
[3] I.M.A. Gledhill, H. Roohani, K. Forsberg, and B.W. Skews. in preparation , 2015.
[4] H. Roohani and B.W. Skews. Shock Waves , 19:297–305, 2009.
[5] T. Saito, K. Hatanaka, H. Yamashita, T. Ogawa, S. Obayashi, and K. Takayama. Shock Waves , 21:483–489, 2011.
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