Blowing Effects on Pressure Interaction Associated With Cones

Schurmann, E.E.H.; Thyson, Noel A.

doi:10.2514/3.2032

Cited by 13 publications

References 4 publications

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Mass Transfer and First-Order Boundary -Layer Effects on Sharp Cone Drag

Lewis¹,

Marchand²,

Little³

1966

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A theoretical model is developed based on an iterated perfect gas inviscid-viscous flow field which includes first-order displacement {viscous interaction), transverse curvature, wall slip, and temperature jump in addition to mass transfer effects. The effects of inviscid (tangent cone) and viscous (nonsimilar laminar boundary layer) flow field matching conditions are also considered. Numerical results are compared with experimental and analytical results of King and Talbot (AI A A J., 1964) for a 5-deg half-angle cone at M" -3. 93 and 5. 64, The predicted viscous-induced pressure without mass transfer and the zero-lift drag with and without injection were in agreement with the experimental data within experimental uncertainty. The theoretical model was also used to predict zero-lift drag of a 9-deg half-angle cone at M^ = 9. 37 and 10 and Re M /in. -400 to 45, 000 for a range of wallto-stagnation temperature ratios. Again, in general, without mass transfer the predictions were within experimental uncertainty. The inability of the theoretical model to adequately treat nonuniform mass transfer distributions is discussed. At the lowest Reynolds number the effects of slip were most significant. At all conditions the effects of inviscid-viscous flow field matching were significant. Experimental zero injection equilibrium wall temperature distributions and cool-wall pressure data are given at M,,,, -10 and Re M /in. = 400 to 2600.in

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