Laminar Reynolds analogy factor on a sharp flat plate at Mach 10.4
Values measured on sharp flat plate in 10.4 Mach boundary layer induced pressure gradient, discussing effects of wall pressure and temperature gradients
Stone, H. W.↗
Engineering topics
Stone, H. W.
Publications and source records attributed to Stone, H. W..
The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4
Stone, H. W.↗
The leading edge effects on a laminar flat- plate boundary layer at Mach 10.4
Leading edge effects on laminar flat-plate boundary layer at Mach 10.4
Stone, H. W.↗
Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4
Roughness effect on heat transfer to hemisphere cylinders in hypersonic flow
HYPERSONIC FLOW↗