The paper describes full-scale balance tests, which have proven structural integrity and longitudinal static stability of an authentic replica of Otto Lilienthal's Large Biplane glider. In addition to that the replica, built after patent drawings, photographs and textual descriptions by the Otto-Lilienthal-Museum, was towed using a rope winch and finally flown downhill without rope or guide wires. The tests allow for the assessment of the aircraft's controllability and stability not only during steady flight, but also during take-off, landing, and on the occasion of wind gusts. A brief description of the design parameters and applied methods is given along with force and moment data gained from balance measurements as well as the evaluation...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Results are presented of an investigation of stability, controllability, and stalling characteristic...
The paper describes full-scale balance tests, which have proven structural integrity and longitudina...
The paper describes successful flight tests using a replica of Otto Lilienthal's patented monoplane ...
The paper describes successful flight tests using a replica of Otto Lilienthal's patented monoplane ...
Successful flight tests with a replica of Otto Lilienthal's patented monoplane glider have been cond...
Free flights as well as winch tows were performed using authentic replicas of Otto Lilienthal's famo...
A full-scale wind tunnel test of a replica of Otto Lilienthal's Normalsegelapparat ("Normal soaring ...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
A mobile experimental test facility has been developed to carry out the aerodynamic evaluation of h...
It was the Wright Brothers who successfully used the process and discipline of flight-test one hundr...
In 1889, Otto Lilienthal published his book Birdflight as the Basis of Aviation, containing the firs...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Results are presented of an investigation of stability, controllability, and stalling characteristic...
The paper describes full-scale balance tests, which have proven structural integrity and longitudina...
The paper describes successful flight tests using a replica of Otto Lilienthal's patented monoplane ...
The paper describes successful flight tests using a replica of Otto Lilienthal's patented monoplane ...
Successful flight tests with a replica of Otto Lilienthal's patented monoplane glider have been cond...
Free flights as well as winch tows were performed using authentic replicas of Otto Lilienthal's famo...
A full-scale wind tunnel test of a replica of Otto Lilienthal's Normalsegelapparat ("Normal soaring ...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
In 1895, Otto Lilienthal patented, built and repeatadly flew a research aircraft equipped with a set...
A mobile experimental test facility has been developed to carry out the aerodynamic evaluation of h...
It was the Wright Brothers who successfully used the process and discipline of flight-test one hundr...
In 1889, Otto Lilienthal published his book Birdflight as the Basis of Aviation, containing the firs...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Results are presented of an investigation of stability, controllability, and stalling characteristic...