Momentum-integral method for calculating subject boundary-layer growth for zero-angle-of-attack case; available flat-plate boundary-layer results permit calculations for cones for wide ranges of hypersonic Mach number and surface temperature; numerical results presented for slender cone show that slight blunting greatly affects conditions at outer edge of boundary layer; Mach number is markedly decreased at long distances from tip; local skin friction and heat transfer are significantly reduced by slight blunting.
Laminar boundary-layer growth on slightly blunted cones at hypersonic speeds
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 2 , n 4
1965
7 pages
Aufsatz (Zeitschrift)
Englisch
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Transition Experiments on Slightly Blunted Cones with Distributed Roughness in Hypersonic Flight
Online Contents | 2012
|TRANSITION EXPERIMENTS ON SLIGHTLY BLUNTED CONES WITH DISTRIBUTED ROUGHNESS IN HYPERSONIC FLIGHT
British Library Conference Proceedings | 2011
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