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.
Structural Flexibility and Undercarriage Impact Loads
The Combination of Landing Reactions and Dynamic Stresses
Aircraft Engineering and Aerospace Technology ; 31 , 5 ; 126-130
1959-05-01
5 pages
Article (Journal)
Electronic Resource
English
Structural flexibility and undercarriage impact loads
Engineering Index Backfile | 1959
|Development of Undercarriage Design Loads
British Library Conference Proceedings | 1991
|Development of Undercarriage Design Loads
NTIS | 1990
|Landing loads on Bogie undercarriage
Engineering Index Backfile | 1952
|Landing Loads on the Bogie Undercarriage
Emerald Group Publishing | 1952
|