Accuracy of pitot-pressure rakes for turbulent boundary-layer measurements in supersonic flow
Accuracy of pitot-pressure rakes for turbulent boundary layer measurement in supersonic flow
Hopkins, E. J.↗
Engineering topics
Keener, E. R.
Publications and source records attributed to Keener, E. R..
Turbulent skin friction and boundary-layer profiles measured on nonadiabatic flat plates at hypersonic Mach numbers
Turbulent skin friction and boundary layer velocity measurements on nonadiabatic flat plates at hypersonic Mach numbers
Dwyer, H. A.↗
Direct measurements of turbulent skin friction on a nonadiabactic flat plate at Mach number 6.5 and comparisons with eight theories
Turbulent skin friction on nonadiabatic flat plate at Mach number 6.5
Hopkins, E. J.↗
Use of Preston tubes for measuring hypersonic turbulent skin friction
Use of Preston tubes for measuring hypersonic turbulent skin friction
Hopkins, E. J.↗
Summary and correlation of skin-friction and heat-transfer data for a hypersonic turbulent boundary layer on simple shapes
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall, and cones
Hopkins, E. J.↗
Use of Preston tubes for measuring hypersonic turbulent skin friction.
Supersonic Preston tube correlations for Mach number and Reynolds number effects on hypersonic turbulent skin friction on adiabatic surfaces, simplifying correlation
Hopkins, E. J.↗
Unit Reynolds number effects on boundary-layer transition at Mach 6.
Boundary layer transition measurement on windward side of flat plate in hypersonic wind tunnel, discussing unit Reynolds number effects at Mach 6
Hopkins, E. J.↗
Study of surface pitots for measuring turbulent skin friction at supersonic Mach numbers - Adiabatic wall
Calibration of surface pitot tubes for measuring turbulent skin friction at supersonic speeds - adiabatic wall
SKIN FRICTION↗
Comments on ''calibration of Preston tubes in supersonic flow.''
Calibration curve for Preston tubes in supersonic flow obtained by reference-temperature method
SUPERSONIC FLOW↗
Flight evaluation of the x-15 ball-nose flow-direction sensor as an air-data system
Modification of ball-nose flow direction sensor for Mach number and air pressure altitude measurements
PRESSURE MEASUREMENT↗
Aerodynamic Forces on Components of the X-15 Airplane
Aerodynamic force data on components of X-15 aircraft obtained by pressure and strain gauge measurements
STRAIN GAUGE↗
Aerodynamic forces on components of the X-15
Explore the source record for details and available documents.
Keener, E. R.↗
Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing
Pressure measurements in flight over conically cambered delta wing of F-102A aircraft at transonic speeds
DELTA WING↗
Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds
Explore the source record for details and available documents.
Jordan, G. H.↗
Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the douglas d-558-i airplane for a 1 g stall, a speed run to a mach number of 0.90, and a wind-up turn at a mach number of 0.86
Explore the source record for details and available documents.
Keener, E. R.↗