Add to ORKGThe effect of several parameters on the drag characteristics of practical-construction wing sections have been considered and evaluated. The effects considered were those of surface roughness, surface waviness, compressive load, and de-icers. The data were obtained from a number of tests in the Langley two-dimensional low-turbulence tunnels
Report presents the results of an investigation conducted in the Langley 19-foot pressure tunnel to ...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
The e$ecte of sereral parameters on the drag characteristics of practical-construction wing section8...
The effect of several parameters on the drag characteristics of practical-construction wing sections...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
In connection with the interference program being conducted in the NACA variable-density wind tunnel...
An investigation has been made to determine the effect of control-surface profile modifications on t...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
In order to obtain a correlation of drag data from wind-tunnel and flight tests at high Mach numbers...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This summary of drag results presents tabulations on fighter aircraft and light twin general aviatio...
A summary of the results of wind-tunnel tests to determine the high-speed aerodynamic characteristic...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Report presents the results of an investigation conducted in the Langley 19-foot pressure tunnel to ...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
The e$ecte of sereral parameters on the drag characteristics of practical-construction wing section8...
The effect of several parameters on the drag characteristics of practical-construction wing sections...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
In connection with the interference program being conducted in the NACA variable-density wind tunnel...
An investigation has been made to determine the effect of control-surface profile modifications on t...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
In order to obtain a correlation of drag data from wind-tunnel and flight tests at high Mach numbers...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This summary of drag results presents tabulations on fighter aircraft and light twin general aviatio...
A summary of the results of wind-tunnel tests to determine the high-speed aerodynamic characteristic...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Report presents the results of an investigation conducted in the Langley 19-foot pressure tunnel to ...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...