Add to ORKGThe first section deals with the theoretical side of statical stability of airships in general. The second section deals with preliminary tests of the model and experiments for the determination of effects due to change of tail area, aspect ratio, tail form, and tail thickness
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
A mobile experimental test facility has been developed to carry out the aerodynamic evaluation of h...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The new method for making computations in connection with the study of rigid airships, which was use...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
The accuracy of the instruments used for flight test measurements has been inadequate so a new serie...
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
A mobile experimental test facility has been developed to carry out the aerodynamic evaluation of h...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The new method for making computations in connection with the study of rigid airships, which was use...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
The accuracy of the instruments used for flight test measurements has been inadequate so a new serie...
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...