Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20
Nozzle wall hypersonic turbulent boundary layers at free stream Mach number, using pitot, hot wire, wall pressure fluctuation and static pressure measurements
Engineering topics
Publications and source records attributed to Wagner, R. D., Jr..
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
Method of characteristics analytical technique for flow predictions of supersonic cross flows over conical bodies
Nozzle wall hypersonic turbulent boundary layers at free stream Mach number using pitot, hot wire, and wall fluctuation and static pressure measurements
Free stream disturbances influence on hypersonic boundary layer transition Reynolds number in heated and unheated flows
Electron beam fluorescence probe and afterglow investigation for hypersonic He flow visualization, observing qualitative structure
Electron beam flow visualization technique for observing low density hypersonic He flows, confirming wing-shock body-shock system existence
Viscous and bluntness induced pressures for flat plates, wedges, cylinders and cones at Mach 41
Viscous and bluntness induced pressures for flat plates, wedges, cylinders and cones at Mach 41
Reynolds number effect on inviscid pressure distributions & shock shapes of cylindrical bodies with different nose shapes & drag coefficients