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.
Tangent-ogive nose cones
NASA Tech Briefs ; 1 , 1
1976-03-01
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Englisch
Tangent ogive nose aerodynamic heating program: NQLD019
NTRS | 1971
|On transonic flow field around tangent ogive bodies
AIAA | 1970
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