Add to ORKGAn analysis has been made of the lift-control effectiveness of a 20-percent-chord plain trailing-edge flap on the NACA 65-210 airfoil section from section lift-coefficient data obtained at Mach numbers from 0.3 to 0.875. In addition, the effectiveness of the plain flap as a lift-control device has been compared with the corresponding effectiveness of both a spoiler and a dive-recovery flag on the INCA 65-210 airfoil section
Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retrac...
Aerodynamic force tests of an NACA 23018 airfoil with a Gwinn flap having a chord 25 percent of the ...
An experimental study was conducted in the Langley Low Turbulence Pressure Tunnel to determine the e...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
This report contains the results of a high-speed wind-tunnel investigation of the effectiveness of a...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
An analysis has been made of the lift-control effectiveness of a 20-percent-chord plain trailing-edg...
Lift and pitching-moment characteristics of an NACA 0006 airfoil are presented for various deflectio...
An investigation has been conducted in the Langley rectangular high-speed tunnel to determine the ef...
Critical Mach number as function of lift coefficient is determined for certain moderately thick NACA...
A summary has been made of available data on the characteristics of airfoil sections with trailing-e...
This report contains the results of a high-speed wind-tunnel investigation of the effectiveness of a...
Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
The effects of wing-lower-surface dive-recovery flaps on the aero- dynamic characteristics of a tran...
Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retrac...
Aerodynamic force tests of an NACA 23018 airfoil with a Gwinn flap having a chord 25 percent of the ...
An experimental study was conducted in the Langley Low Turbulence Pressure Tunnel to determine the e...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
This report contains the results of a high-speed wind-tunnel investigation of the effectiveness of a...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
An analysis has been made of the lift-control effectiveness of a 20-percent-chord plain trailing-edg...
Lift and pitching-moment characteristics of an NACA 0006 airfoil are presented for various deflectio...
An investigation has been conducted in the Langley rectangular high-speed tunnel to determine the ef...
Critical Mach number as function of lift coefficient is determined for certain moderately thick NACA...
A summary has been made of available data on the characteristics of airfoil sections with trailing-e...
This report contains the results of a high-speed wind-tunnel investigation of the effectiveness of a...
Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
The effects of wing-lower-surface dive-recovery flaps on the aero- dynamic characteristics of a tran...
Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retrac...
Aerodynamic force tests of an NACA 23018 airfoil with a Gwinn flap having a chord 25 percent of the ...
An experimental study was conducted in the Langley Low Turbulence Pressure Tunnel to determine the e...