Numerical simulation of aircraft arresting process with an efficient full-scale rigid-flexible coupling dynamic model

Author:

SHAO Haoyuan,LI Daochun,KAN ZiORCID,BI Lanxi,YAO Zhuoer,XIANG Jinwu

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

Elsevier BV

Reference26 articles.

1. A review of civil aircraft arresting system for runway overruns;Yang;Prog Aerosp Sci,2018

2. Dynamics test research of bounce of carrier-based aircraft arresting hook;Peng;Appl Sci,2020

3. Naval Air Engineering Center. Military standard: Catapulting and arresting gear forcing functions for aircraft structural design. Washington, D.C.: Department of the Navy Air Systems Command; 1981. Standard No.: MIL-STD-2066. p. 108–70.

4. Naval Air Systems Command. Airplane strength and rigidity: Ground loads for carrier-based aircraft. Washington, D.C.: Naval Air Systems Command; 1993. Standard No.: MIL-A-8863C.

5. Thomlinson J. A study of the aircraft arresting-hook bounce problem. The principal director of scientific research (air). London; 1954.

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