Verification of a mathematical model of dynamic loading in the quasistatic statement for a helicopter tubular skid landing gear by the results of drop tests

被引：0

作者：

S. A. Mikhailov

D. V. Nedel’ko

L. V. Korotkov

S. A. Alimov

机构：

[1] Tupolev Kazan National Research Technical University,

[2] OAO Kazan Helicopters,undefined

来源：

Russian Aeronautics (Iz VUZ) | 2012年 / 55卷 / 3期

关键词：

drop; model; center of gravity; skid landing gear; landing; tensometric platform, experiment; drop tests; model;

D O I：

10.3103/S1068799812030026

中图分类号：

学科分类号：

摘要：

We present the results of verifying a mathematical model of dynamic loading of the helicopter skid landing gear with regard for two successive landing impacts. Also presented are the results of analyzing the interaction of springs in the course of drop tests.

引用

页码：230 / 232

页数：2

共 5 条

[1] Mathematical model of helicopter landing with skid landing gear
Mikhailov, SA
Nedel'ko, DV
Nikolaev, EI
IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 2001, (01): : 8 - 12
[2] Analysis of static loading of a helicopter tubular skid landing gear
Mikhailov S.A.
Korotkov L.V.
Nedel’ko D.V.
Russian Aeronautics, 2010, 53 (04): : 369 - 374
[3] Analysis of static loading for a helicopter tubular skid landing gear
S. A. Mikhailov
L. V. Korotkov
D. V. Nedel’ko
Russian Aeronautics (Iz VUZ), 2012, 55 (4) : 348 - 352
[4] Efficient helicopter skid landing gear dynamic drop simulation using LS-DYNA
Tho, CH
Sparks, CE
Sareen, AK
Smith, MR
Johnson, C
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2004, 49 (04) : 483 - 492
[5] Dynamic analysis of an SDOF helicopter model featuring skid landing gear and an MR damper by considering the rotor lift factor and a Bingham number
Saleh, Muftah
Sedaghati, Ramin
Bhat, Rama
SMART MATERIALS AND STRUCTURES, 2018, 27 (06)

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