This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and dihedral on some of the aerodynamic characteristics of Clark Y wings that affect the performance and lateral stability of airplanes. Force tests at several angles of yaw and rotation tests at zero yaw were made. From these tests the rates of change of rolling moment, yawing moment, and cross-wind force coefficients with angle of yaw and the rate of change of rolling moment coefficient with rolling were determined
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
Tests have been made in the NACA 7 by 10 foot wind tunnel on a Clark Y wing model equipped with vari...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
An investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the eff...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
Four N.A.C.A. 23012 wings were tested at several an-gles of yaw in the N.A.G.A. 7- by lo-foot gind t...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Tests showed the effect of the ailerons and the tip shapes on the general performance of the wing, a...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
Dihedral and sweep back can properly be compared only to the extent to which their action is similar...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
Tests have been made in the NACA 7 by 10 foot wind tunnel on a Clark Y wing model equipped with vari...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
An investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the eff...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
Four N.A.C.A. 23012 wings were tested at several an-gles of yaw in the N.A.G.A. 7- by lo-foot gind t...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Tests showed the effect of the ailerons and the tip shapes on the general performance of the wing, a...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
Dihedral and sweep back can properly be compared only to the extent to which their action is similar...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
Tests have been made in the NACA 7 by 10 foot wind tunnel on a Clark Y wing model equipped with vari...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...