Add to ORKGIn connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the formal results are here amplified in some respects and their technical significance again briefly explained. Three numerical examples show how model tests for checking the lateral stability are to be evaluated and supplemented, if necessary, and how the stability limits depend on the design of the airplane and on the conditions of flight
The effects of large variations of lateral area on the lateral stability and control characteristics...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
The aerodynamic and mass factors governing lateral stability are discussed and formulas are given fo...
An investigation has been made of a complete airplane model having a wing with the quarter-chord lin...
The results of the computations are presented in the form of diagrams of variations of fin area with...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
The effects of large variations of lateral area on the lateral stability and control characteristics...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
The aerodynamic and mass factors governing lateral stability are discussed and formulas are given fo...
An investigation has been made of a complete airplane model having a wing with the quarter-chord lin...
The results of the computations are presented in the form of diagrams of variations of fin area with...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
The effects of large variations of lateral area on the lateral stability and control characteristics...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The results of an experimental and theoretical investigation of the effects of large artificial vari...