Add to ORKGAn investigation was made in the LWAL 7- by 10-foot tunnel of internally balanced, sealed ailerons for the Curtiss XP-60 airplane. Ailerons with tabs and. with various amounts of balance were tested. Stick forces were estimated for several aileron arrangements including an arrangement recommended for the airplane. Flight tests of the recommended arrangement are discussed briefly in an appendix, The results of the wind-tunnel and flight tests indicate that the ailerons of large or fast airplanes may be satisfactorily balanced by the method developed
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
Investigations were undertaken to improve the ailerons of a P-51 fighter so as to obtain greater eff...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane wit...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
An investigation was made in the LMAL 7- by 10-foot tunnel of various modifications to the trailing ...
Flight measurements have been made to determine the characteristics of a pair of experimental ailero...
A flight investigation was made of the increase in effectiveness of ailerons that can be obtained by...
Ailerons having a beveled trailing edge and a blunt-nose overhang of 35 percent aileron chord on an ...
This paper presents the results of the aileron investigation and includes rolling-moment, yawing-mom...
An investigation has been conducted in the Langley 4- by 4-foot supersonic tunnel at Mach numbers 1....
The failure of wing panels on a number of TBF-1 and TBM-1 airplanes in flight has prompted several i...
The aileron characteristics of a Grumman F4F-3 airplane were determined in flight by means of NACA r...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
Investigations were undertaken to improve the ailerons of a P-51 fighter so as to obtain greater eff...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane wit...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
An investigation was made in the LMAL 7- by 10-foot tunnel of various modifications to the trailing ...
Flight measurements have been made to determine the characteristics of a pair of experimental ailero...
A flight investigation was made of the increase in effectiveness of ailerons that can be obtained by...
Ailerons having a beveled trailing edge and a blunt-nose overhang of 35 percent aileron chord on an ...
This paper presents the results of the aileron investigation and includes rolling-moment, yawing-mom...
An investigation has been conducted in the Langley 4- by 4-foot supersonic tunnel at Mach numbers 1....
The failure of wing panels on a number of TBF-1 and TBM-1 airplanes in flight has prompted several i...
The aileron characteristics of a Grumman F4F-3 airplane were determined in flight by means of NACA r...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
Investigations were undertaken to improve the ailerons of a P-51 fighter so as to obtain greater eff...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...