Add to ORKGThe discussion of the structural methods for obtaining lateral stability discloses the remarkable influence of the constant fuselage and wing proportions to the yawing moments. For the effectiveness of modifications in vertical tail surfaces and tail length, these quotas - little observed heretofore, in this connection - are decisive. This also applies to the amount of dihedral of the wing with regard to the roll stability of the complete wing already existing without angle of the dihedral
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
This report presents the results of an analytical study of the lateral controllability of an airplan...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
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...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
This report presents the results of an analytical study of the lateral controllability of an airplan...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
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...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
This report presents the results of an analytical study of the lateral controllability of an airplan...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...