Engineering topics
Publications and source records attributed to Maddalon, D. V..
Nozzle wall hypersonic turbulent boundary layers at free stream Mach number, using pitot, hot wire, wall pressure fluctuation and static pressure measurements
Free stream disturbances influence on hypersonic boundary layer transition Reynolds number in heated and unheated flows
Thermal conductivity and viscosity of helium at high Mach number wind tunnel conditions
Nozzle wall hypersonic turbulent boundary layers at free stream Mach number using pitot, hot wire, and wall fluctuation and static pressure measurements
Correction factor for free stream Reynolds number errors resulting from low temperature viscosity in He wind tunnels
Wall and total temperature variations effects on transition Reynolds number in hypersonic He tunnel, noting sound mode dominance
Free stream disturbances influence on hypersonic boundary layer transition Reynolds number in heated and unheated flows
Wind tunnel tests on pressure distribution, and shock shapes of conical blunted bodies moving at supersonic speeds in nitrogen, or helium media
Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Angle of attack effect on laminar boundary layer transition on slender cone in contoured nozzle of helium tunnel, discussing Reynolds and Mach numbers effect
Boundary layer transition measurements of contoured nozzle flow at hypersonic Mach numbers
Transition from laminar to turbulent boundary layer flow at hypersonic Mach numbers, noting measurement techniques
Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach numbers, including Reynolds number effect
Static longitudinal aerodynamic characteristics of sharp right circular cone at Mach 20.3 and angles of attack to 110 deg in helium