Add to ORKGA theoretical method is presented for predicting the lateral-directional stability derivatives of wing-body combinations with or without the blowing jet effect. The fuselage effect is accounted for by the axial distribution of vortex multiplets. Comparison of the predicted results with experiments and other theoretical methods show good agreement for configurations without the blowing jet. More applicable experimental data with blowing jets are needed to establish the accuracy of the theory
Low-speed, static wind-tunnel tests were conducted to explore the effects of fighter fuselage forebo...
The concept of lateral blowing consists in utilizing thin jets of air, which are ejected in the span...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
An investigation has been conducted to determine the effects of configuration variables on the later...
The nonplanar quasi-vortex-lattice method is applied to the calculation of lateral-directional stabi...
A study of some of the important aerodynamic factors affecting the directional stability of superson...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A computer program based on the Quasi-Vortex-Lattice Method of Lan is presented for calculating long...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
A small-disturbance theory is developed for predicting the aerodynamics of an airplane in sideslip. ...
A theoretical method is presented for determining the optimum camber shape and twist distribution fo...
Low-speed, static wind-tunnel tests were conducted to explore the effects of fighter fuselage forebo...
The concept of lateral blowing consists in utilizing thin jets of air, which are ejected in the span...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
An investigation has been conducted to determine the effects of configuration variables on the later...
The nonplanar quasi-vortex-lattice method is applied to the calculation of lateral-directional stabi...
A study of some of the important aerodynamic factors affecting the directional stability of superson...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
Experimentally determined lateral-stability derivatives of a swept-wing airplane are presented to sh...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
A computer program based on the Quasi-Vortex-Lattice Method of Lan is presented for calculating long...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
A small-disturbance theory is developed for predicting the aerodynamics of an airplane in sideslip. ...
A theoretical method is presented for determining the optimum camber shape and twist distribution fo...
Low-speed, static wind-tunnel tests were conducted to explore the effects of fighter fuselage forebo...
The concept of lateral blowing consists in utilizing thin jets of air, which are ejected in the span...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...