NASA NTRS · 19760000107
Tangent-ogive nose cones
Abstract
Program calculates aerodynamic heating and shear stresses at wall for tangent-ogive noses that are slender enough to maintain an attached nose shock during portion of flight when heat transfer from boundary layer to wall is significant.
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Wing, L. D.. 1976-03-01. Tangent-ogive nose cones. https://ntrs.nasa.gov/citations/19760000107
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