TY  - JOUR
AB  - THE present paper gives, in abbreviated form, the theory of blade motion and of static and dynamic stability of single‐rotor helicopters. Limitations of space do not permit of full discussion and the article should be taken as only an introduction to the somewhat complex problems of helicopter stability and control.
VL  - 21
IS  - 2
SN  - 0002-2667
DO  - 10.1108/eb031724
UR  - https://doi.org/10.1108/eb031724
AU  - Zbrozek J.K.
PY  - 1949
Y1  - 1949/01/01
TI  - Stability and Control of Single Rotor Helicopter with Hinged Blades: A Statement of the Elements of a Complex Subject in which the Author has Presented the Case with the Minimum Use of Mathematics
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 32
EP  - 38
Y2  - 2024/04/23
ER  -