Turbulent skin friction and heat-transfer charts adapted from the Spalding and Chi method
Local and average skin friction and heat transfer on flat plates in air - charts
SKIN FRICTION↗
Engineering topics
Neal, L., Jr.
Publications and source records attributed to Neal, L., Jr..
Hypersonic performance of several basic and modified diamond cross-section delta wing configurations
Hypersonic flight performance of basic and modified delta wings with diamond cross sections
DIAMOND WING↗
Average pressure and skin friction on tapered plates in hypersonic flow.
Average pressure and skin friction on slender two- dimensional wings in hypersonic flow, taking into account displacement effects of boundary layer
SLENDER WING↗
A study of the pressure, heat transfer, and skin friction on sharp and blunt flat plates at Mach 6.8
Pressure, heat transfer, and skin friction studies on sharp and blunt flat plates at hypersonic speeds
FLAT PLATE↗
Aerodynamic characteristics of two trailblazer ii blunted 9 deg cone reentry bodies at mach 6.8 in air and 21.2 in helium
Effect of aerodynamic characteristics of nose bluntness on electromagnetic and luminous efficiency by comparing radar and optical data of two reentry bodies at escape velocities
REENTRY BODY↗
Recent experiments in hypersonic turbulent boundary layers
Hypersonic turbulent boundary layer experiments - skin friction, heat transfer, shear stress on flat plates and cones, and boundary layer velocity and thermal profiles on nozzle walls
VELOCITY PROFILE↗
AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 6.77 OF A 9 DEG CONE CONFIGURATION, WITH AND WITHOUT SPHERICAL AFTERBODIES, AT ANGLES OF ATTACK UP TO 180 DEG WITH VARIOUS DEGREES OF NOSE BLUNTING
Aerodynamic characteristics at mach 6.77 of 9-deg cone, with and without spherical afterbody and nose blunting at angles of attack to 180-deg
AFTERBODY↗