Measurements of shock wave location in hypersonic nitrogen flow
Complex three dimensional shock waves about space shuttle configuration, visualizing hypersonic nitrogen flow with electron beams
Emory, M. L.↗
Engineering topics
Harvey, W. D.
Publications and source records attributed to Harvey, W. D..
Comparisons of turbulent-boundary-layer measurements at Mach number 19.5 with theory and an assessment of probe errors
Measurements of total temperature and pitot pressure across boundary layer of test section wall of axisymmetric contoured nozzle at hypersonic speed in nitrogen
Beckwith, I. E.↗
Fluctuating properties of turbulent boundary layers for Mach numbers up to 9
Fluctuating properties of turbulent boundary layers for Mach numbers up to 9
Beckwith, I. E.↗
Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls
Bushnell, D. M.↗
Velocity fluctuation intensities in a hypersonic turbulent boundary layer.
Density and velocity fluctuations in hypersonic turbulent boundary layer based on Wallace data
Bushnell, D. M.↗
Experimental investigation of laminar-flow separation on a flat plate induced by deflected trailing-edge flap at Mach 19
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic speed
Harvey, W. D.↗
Heat sensing instrument Patent
Heat sensing instrument, using thermocouple junction connected under heavy conducting material
Harvey, W. D.↗
Instrumenting models for aerodynamic heat- transfer studies involving transient heating rates.
Instrumenting techniques for models under aerodynamic transient heating
INSTRUMENT PACKAGE↗
Instrument accurately measures small temperature changes on test surface
Calorimeter apparatus accurately measures very small temperature rises on a test surface subjected to aerodynamic heating. A continuous thin sheet of a sensing material is attached to a base support plate through which a series of holes of known diameter have been drilled for attaching thermocouples to the material.
Harvey, W. D.↗
Effects of leading-edge bluntness on pressure and heat-transfer measurements over a flat plate at a mach number of 20
Effects of leading edge bluntness on pressure and heat transfer at hypersonic speed
HEAT TRANSFER↗
Continuous skin construction technique for fabricating models for aerodynamic heat- transfer studies involving very small transient heating rates
Instrumentation technique for simple or complicated shapes for measuring aerodynamic heat transfer in hotshot tunnel
INSTRUMENTATION↗