Add to ORKGThis survey is intended to give a general approximate idea of the stability and controllability of German airplanes
Measurements of the longitudinal stability and control of a pursuit-type airplane were made in fligh...
The notion of airplane stability and control being a balancing act between stability and control ha...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
The author attempts to correct the misconception that piloting an airplane requires extraordinary sk...
This report describes the development of airplane characteristics since the war and indicates the di...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The author, who was a captain of the Reserves in the Technical Department of the Aviation Division (...
Our task is to endeavor to obtain precise experimental records of the motion of stalled airplanes, b...
This report outlines the flight conditions that are usually critical in determining the design of co...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The development of more efficient control surfaces requiring less force to operate are presented
The authors argue that the center of gravity has a preponderating influence on the longitudinal stab...
Measurements of the longitudinal stability and control of a pursuit-type airplane were made in fligh...
The notion of airplane stability and control being a balancing act between stability and control ha...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
The author attempts to correct the misconception that piloting an airplane requires extraordinary sk...
This report describes the development of airplane characteristics since the war and indicates the di...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The author, who was a captain of the Reserves in the Technical Department of the Aviation Division (...
Our task is to endeavor to obtain precise experimental records of the motion of stalled airplanes, b...
This report outlines the flight conditions that are usually critical in determining the design of co...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
The development of more efficient control surfaces requiring less force to operate are presented
The authors argue that the center of gravity has a preponderating influence on the longitudinal stab...
Measurements of the longitudinal stability and control of a pursuit-type airplane were made in fligh...
The notion of airplane stability and control being a balancing act between stability and control ha...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...