Add to ORKGTurbulent boundary layer of subsonic transport fuselage with pressure gradient, Reynolds number, and angle of attac
Base and afterbody pressures on boattailed bodies of revolution with hypersonic turbulent boundary l...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...
An investigation has been made in the Langley full-scale tunnel to determine the thickness and shape...
Analyses have been conducted of wing pressure distribution and boundary layer data obtained from fli...
This report describes the equipment and method developed for recording the boundary layers on the su...
Transonic wind tunnel studies on airfoil to determine effects of Reynolds number and boundary layer ...
Boundary layer characteristics of fuselages of various cross sectional shapes at static pressur
The effect of the existing turbulence in the full scale tunnel was determined from measurements of t...
A summary report of boundary layer studies is presented. Preliminary results of experimental measure...
Measurements of base pressure are presented for 29 blunt-trailing-edge wings having an aspect ratio ...
Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at ...
Experimental studies of a two and a three-dimensional low speed turbulent boundary layer were conduc...
Surface roughness effects on boundary layer transition indicated by thermocouple data from X-15 airc...
An experimental investigation is being conducted to evaluate the boundary layer associated with a tw...
Base and afterbody pressures on boattailed bodies of revolution with hypersonic turbulent boundary l...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...
An investigation has been made in the Langley full-scale tunnel to determine the thickness and shape...
Analyses have been conducted of wing pressure distribution and boundary layer data obtained from fli...
This report describes the equipment and method developed for recording the boundary layers on the su...
Transonic wind tunnel studies on airfoil to determine effects of Reynolds number and boundary layer ...
Boundary layer characteristics of fuselages of various cross sectional shapes at static pressur
The effect of the existing turbulence in the full scale tunnel was determined from measurements of t...
A summary report of boundary layer studies is presented. Preliminary results of experimental measure...
Measurements of base pressure are presented for 29 blunt-trailing-edge wings having an aspect ratio ...
Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at ...
Experimental studies of a two and a three-dimensional low speed turbulent boundary layer were conduc...
Surface roughness effects on boundary layer transition indicated by thermocouple data from X-15 airc...
An experimental investigation is being conducted to evaluate the boundary layer associated with a tw...
Base and afterbody pressures on boattailed bodies of revolution with hypersonic turbulent boundary l...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...