The present report deals with the aerodynamic, constructive, and instrumental development of a spoiler control for remote control of flying missiles
Paper presenting three ideas regarding potential simplifications of missile-control systems in order... Read more
Results of an investigation at low speeds to determine the gust-alleviation capabilities (reduction ... Read more
This report presents the results of flight tests made to determine the lateral control characteristi... Read more
The present report describes the development of spoiler control at the DVL from the end of 1936 unti... Read more
Add to ORKG