Static pressure measurements near an oblique shock wave
Static pressure measurements near oblique shock waves using short probe, evaluating readings accuracy
Back, L. H.↗
Engineering topics
Back, L. H.
Publications and source records attributed to Back, L. H..
Relationship between temperature and velocity profiles in a turbulent boundary layer along a supersonic nozzle with heat transfer
Turbulent boundary layer air flow through supersonic convergent-divergent nozzle with heat transfer, considering relationship between temperature and velocity profiles
Back, L. H.↗
Changes in heat transfer from turbulent boundary layers interacting with shock waves and expansion waves
Heat transfer from turbulent boundary layer interacting with shock and expansion waves in supersonic flow
Back, L. H.↗
Effect of wall cooling on the mean structure of a turbulent boundary layer in low-speed gas flow
Wall cooling effects on turbulent boundary layer in low speed air flow, using smooth tube and thermocouple measurements
Back, L. H.↗
Acceleration and cooling effects in laminar boundary layers - Subsonic, transonic, and supersonic speeds
Subsonic, transonic and supersonic laminar boundary layers acceleration and cooling effects, discussing heat transfer and gas enthalpy
Back, L. H.↗
Viscous effects on the flow coefficient for a supersonic nozzle
Adiabatic flow coefficient in supersonic nozzle with choked flow conducted over throat Reynolds number range
Back, L. H.↗
Experimental convective heat transfer and pressure distributions and boundary layer thicknesses in turbulent flow through a variable cross-sectional area channel
Wall static pressure and convective heat transfer measurements in subsonic, transonic and supersonic regions in heated air turbulent flow through variable cross section channel
Back, L. H.↗
Flow and heat transfer in laminar boundary layers with swirl.
Superimposed free vortex swirl effect on flow and heat transfer in three dimensional axisymmetric laminar boundary layer
Back, L. H.↗
Laminarization of a turbulent boundary layer in nozzle flow - Boundary layer and heat transfer measurements with wall cooling.
Boundary layer and heat transfer measurements for turbulent boundary layer laminarizing in conical nozzle flow with wall cooling
Back, L. H.↗
Laminar, transition, and turbulent boundary- layer heat-transfer measurements with wall cooling in turbulent airflow through a tube.
Laminar, transition and turbulent boundary layer heat transfer measurements along wall in thermal entrance region of high temperature turbulent airflow through cooled tube
Back, L. H.↗
Transonic flowfield in a supersonic nozzle with small throat radius of curvature.
Internal flow measurements in transonic region of supersonic nozzle with small throat radius of curvature compared with prediction data
Back, L. H.↗
Laminarization of a turbulent boundary layer in nozzle flow.
Turbulent boundary layer laminarization in conical nozzle flow, measuring velocity profiles and friction coefficient
Back, L. H.↗
Heat transfer and laminar boundary-layer distributions in an internal subsonic gas stream at temperatures up to 13,900 deg R.
Velocity, enthalpy and mass flux radial distributions in laminar boundary layer from calorimetry of argon subsonic flow
Back, L. H.↗
Flow and heat-transfer measurements in subsonic air flow through a contraction section.
Flow and heat transfer measurements for heated air in subsonic flow through contraction section connecting tube to conical section
Back, L. H.↗
Laminar heat transfer in electrically conducting fluids flowing in parallel plate channels.
Laminar heat transfer in electrically conducting fluids flowing in parallel plate channels
Back, L. H.↗
Effects of surface cooling and heating on structure of low-speed, laminar boundary-layer gas flows with constant free-stream velocity.
Surface cooling and heating effects on low speed laminar boundary layer gas flow with constant free stream velocity
Back, L. H.↗
Heat transfer and laminar boundary-layer distributions in an internal subsonic gas stream at temperatures up to 13,900 deg R.
Velocity, enthalpy and mass flux radial distributions in laminar boundary layer from calorimetry of argon subsonic flow
Back, L. H.↗
Heat-transfer measurements in the shock-induced flow separation region in a supersonic nozzle.
Pressure and semilocal wall heat flux measurements in shock induced flow separation region in supersonic nozzle, noting shock waves-flow interaction
Back, L. H.↗