TY  - JOUR
AB  - The calculation of undercarriage landing reactions and dynamic stresses is discussed, and the merging of the two calculations under certain circumstances is proposed. ? formulation of the combined problem is outlined, and numerical examination of a simple case shows that in some cases the reaction forces are appreciably reduced by the adoption of the combined approach. Finally, a criterion is derived which could be used in the early stages of undercarriage design to predict the elicci of aircraft flexibility.
VL  - 31
IS  - 5
SN  - 0002-2667
DO  - 10.1108/eb033111
UR  - https://doi.org/10.1108/eb033111
AU  - Alexander H.R.
PY  - 1959
Y1  - 1959/01/01
TI  - Structural Flexibility and Undercarriage Impact Loads: The Combination of Landing Reactions and Dynamic Stresses
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 126
EP  - 130
Y2  - 2024/04/24
ER  -