TY  - JOUR
AB  - In Part 1 it is shown that the equation for blade equilibrium about the flapping pin is
VL  - 26
IS  - 2
SN  - 0002-2667
DO  - 10.1108/eb032391
UR  - https://doi.org/10.1108/eb032391
AU  - Payne P.R.
PY  - 1954
Y1  - 1954/01/01
TI  - Rotor Blade Motion in a Vertical Sharp‐edged Gust: A Study of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 41
EP  - 45
Y2  - 2024/04/25
ER  -