Conference on Physics of Entry Into Planetary Atmospheres 1963
DOI: 10.2514/6.1963-434
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Hypersonic Viscous Drag Effects on Blunt Slender Cones

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(3 citation statements)
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“…[1][2][3]. The large viscousinduced drag increment at zero-lift observed in these studies encouraged Whitfield and Griffith (Ref.…”
mentioning
confidence: 69%
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“…[1][2][3]. The large viscousinduced drag increment at zero-lift observed in these studies encouraged Whitfield and Griffith (Ref.…”
mentioning
confidence: 69%
“…Therefore for more direct comparison with King and Talbot, v e /u e = dSVdx (1)(2)(3) was used in most of the calculations. The inviscid flow field was computed from the approximate tangent cone theory.…”
Section: Aedc-tr-66-37mentioning
confidence: 99%
“…The axial force may be related to the drag coefficient by using the body axes as a reference : CA = CD cosa -CL sina (5) and for small a, CA = CD. Consideration must also be given to skin-friction drag; in general, the average skin friction in a laminar boundary layer maybe expressed as C F = CiRe L~1 12 .…”
mentioning
confidence: 99%