Effect of inlet boundary-layer thickness and structure on heat transfer in a supersonic nozzle.
Inlet boundary layer thickness and structure effects on heat transfer in supersonic nozzle
Back, L. H.↗
Engineering topics
Back, L. H.
Publications and source records attributed to Back, L. H..
Flow phenomena and convective heat transfer in a conical supersonic nozzle.
Turbulent boundary layer flow in conical supersonic nozzle, discussing convective heat transfer and adverse pressure gradient effect
GAS DYNAMICS↗
Laminar boundary-layer heat transfer from a partially ionized monatomic gas.
Similarity solution to laminar boundary layer heat transfer from monatomic gas to cooled wall with no applied electric or magnetic fields
GAS FLOW↗
Detection of oblique shocks in a conical nozzle with a circular-arc throat.
Oblique shock detection in conical nozzle with circular arc throat, noting measurement techniques
CONICAL NOZZLE↗
Some observations on reduction of turbulent boundary-layer heat transfer in nozzles.
Convective heat transfer in accelerated heated air flows through cooled conical supersonic nozzles of three different configurations
AIRFLOW↗
Prediction of heat transfer from laminar boundary layers, with emphasis on large free- stream velocity gradients and highly cooled walls.
Laminar boundary-layer heat transfer and shear stress predictions from similarity solutions, emphasizing large free-stream velocity gradients and highly cooled walls
SHEARING STRESS↗
Laminar boundary-layer heat transfer from a partially-ionized monatomic gas by the similarity approach
Laminar boundary layer heat transfer from ionized monatomic gas to wind tunnel wall
IONIZED GAS↗
Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic region.
Measured and predicted flows through conical supersonic nozzles compared, emphasizing transonic region
SUPERSONIC NOZZLE↗
Prediction of heat transfer from laminar boundary layers, with emphasis on large free- stream velocity gradients and highly cooled walls.
Laminar boundary-layer heat transfer and shear stress predictions from similarity solutions, emphasizing large free-stream velocity gradients and highly cooled walls
STAGNATION POINT↗
Prediction of heat transfer from laminar boundary layers, with emphasis on large free- stream velocity gradients and highly cooled walls
Prediction of heat transfer and shear stress from laminar boundary layer
HEAT TRANSFER↗
Convective heat transfer in a convergent- divergent nozzle
Convective heat transfer from turbulent boundary layer in convergent-divergent conical nozzle
DIVERGENT NOZZLE↗
Comparisons of experimental with predicted wall static-pressure distributions in conical supersonic nozzles
Experimental and predicted wall static-pressure distributions in conical supersonic nozzles
CONICAL NOZZLE↗
On constant property turbulent boundary layers with variable temperature or heat flow at the wall.
Heat transfer to turbulent boundary layer, using Spalding form of thermal energy equation
THERMAL ENERGY↗
Convective heat transfer in a convergent- divergent nozzle.
Convective heat transfer investigated for turbulent boundary layer flow through cooled convergent-divergent nozzle
CONVECTIVE HEAT TRANSFER↗
Convective heat transfer in a convergent- divergent nozzle
Turbulent flow convective heat transfer in convergent-divergent nozzles
CONVERGENT-DIVERGENT NOZZLE↗