A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption
Crossref DOI link: https://doi.org/10.3103/S1068799818020058
Published Online: 2019-01-19
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Nedel’ko, D. V.
Alimov, S. A.
Text and Data Mining valid from 2018-04-01
Article History
Received: 7 September 2017
First Online: 19 January 2019