Add to ORKGSectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retractable ailerons are presented for a large range of aileron deflections. The analysis indicated that pitching moments produced by spoilers were less positive than those produced by plain flaps of equal effectiveness, also that pitching moments created by the spoiler increased less with the Mach number than similar moments produced by plain flaps. Positive values of pitching moment decreased as devices were located nearer airfoil leading edge
Compressibilit:y effects on.the aerodynanic section characteristics of an airfoil with a round-nose ...
Force and surface pressure distributions were measured for the 21% LS(1)-0421 modified airfoil fitte...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retrac...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Tests were made of an 0.309-chord double-slotted flap on an NACA 65, 3-118, a equals 1.0 airfoil sec...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
This paper present results of an investigation of the lateral-control and hinge-moment characteristi...
A summary has been made of available data on the characteristics of airfoil sections with trailing-e...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
An experimental study has been carried out on an airfoil with slotted flap and spoiler using Joukows...
An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional ...
A rapidly deployed spoiler on the upper surface of a wing induces adverse lift and moment during air...
Compressibilit:y effects on.the aerodynanic section characteristics of an airfoil with a round-nose ...
Force and surface pressure distributions were measured for the 21% LS(1)-0421 modified airfoil fitte...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retrac...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Tests were made of an 0.309-chord double-slotted flap on an NACA 65, 3-118, a equals 1.0 airfoil sec...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
This paper present results of an investigation of the lateral-control and hinge-moment characteristi...
A summary has been made of available data on the characteristics of airfoil sections with trailing-e...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
An experimental study has been carried out on an airfoil with slotted flap and spoiler using Joukows...
An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional ...
A rapidly deployed spoiler on the upper surface of a wing induces adverse lift and moment during air...
Compressibilit:y effects on.the aerodynanic section characteristics of an airfoil with a round-nose ...
Force and surface pressure distributions were measured for the 21% LS(1)-0421 modified airfoil fitte...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
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