Engineering topics
Publications and source records attributed to Jones, R. A..
Variable density hypervelocity wind tunnel tests on effects of several ramp-fairing, umbilical, and pad configurations on aerodynamic heating to Apollo command module
Blunt body with constant surface pressure gradient for boundary layer transition studies, deriving body shape with Newtonian theory for local pressures
Boundary layer transition point on forward portion of blunt Apollo type entry capsule model measured in high Reynolds number wind tunnel
Flow field, pressure distributions, and heat transfer distribution of several tension shell configurations at hypersonic speeds
Measuring aerodynamic heating of wind-tunnel models by temperature sensitive paint, noting ambient pressure effect
Fusible thin film coatings used in determining aerodynamic heat transfer coefficients at hypersonic speeds
Phase change photographs used for quantitative aerodynamic heat transfer data with surface coating materials
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Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg