A summary of methods for making dynamic lateral stability and response calculations and for estimating the aerodynamic stability derivatives required for use in these calculations is presented. The processes of performing calculations of the time histories of lateral motions, of the period and damping of these motions, and of the lateral stability boundaries are presented as a series of simple straightforward steps. Existing methods for estimating the stability derivatives are summarized and, in some cases, simple new empirical formulas are presented. Detailed estimation methods are presented for low-subsonic-speed conditions but only a brief discussion and a list of references are given for transonic and supersonic speed conditions
Aerodynamic longitudinal damping derivatives are of great importance for aircraft stability and cont...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A method is presented for determining the lateral-stability derivatives, transfer-function coefficie...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
Several new systematic methods for high fidelity and reliability calculation of static and single dy...
Contains derivations, based on a simplified theory, of approximate relations for low-speed stability...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A summary of methods for making dynamic lateral stability and response calculations and for estimati...
The motivation behind the inclusion of unsteady aerodynamics and aeroelastic effects in the computat...
Aerodynamic longitudinal damping derivatives are of great importance for aircraft stability and cont...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A method is presented for determining the lateral-stability derivatives, transfer-function coefficie...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
Several new systematic methods for high fidelity and reliability calculation of static and single dy...
Contains derivations, based on a simplified theory, of approximate relations for low-speed stability...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A summary of methods for making dynamic lateral stability and response calculations and for estimati...
The motivation behind the inclusion of unsteady aerodynamics and aeroelastic effects in the computat...
Aerodynamic longitudinal damping derivatives are of great importance for aircraft stability and cont...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...