TY - JOUR
T1 - Comparison Virtual Landing Gear Drop Test for Commuter Aircraft Utilize MSC ADAMS and Solidworks Motion Analysis
AU - Hidayat, Dony
AU - Istiyanto, Jos
AU - Sumarsono, Danardono Agus
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2018/5/4
Y1 - 2018/5/4
N2 - Loads at main landing gear while touchdown impact is function of aircraft weight and ground reaction load factor. In regulation states ground reaction load factor at Vsink = 3.05 m/s is below 3. Contact/impact force from simulation using MSC ADAMS is 94680 N, while using Solidworks Motion Analysis is 97691 N. The difference between MSC ADAMS and Solidworks Motion Analysis is 3.08%. The ground reaction load factor in MSC ADAMS is 2.78 while in Solidworks Motion Analysis is 2.87.
AB - Loads at main landing gear while touchdown impact is function of aircraft weight and ground reaction load factor. In regulation states ground reaction load factor at Vsink = 3.05 m/s is below 3. Contact/impact force from simulation using MSC ADAMS is 94680 N, while using Solidworks Motion Analysis is 97691 N. The difference between MSC ADAMS and Solidworks Motion Analysis is 3.08%. The ground reaction load factor in MSC ADAMS is 2.78 while in Solidworks Motion Analysis is 2.87.
UR - http://www.scopus.com/inward/record.url?scp=85047734914&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1005/1/012007
DO - 10.1088/1742-6596/1005/1/012007
M3 - Conference article
AN - SCOPUS:85047734914
SN - 1742-6588
VL - 1005
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012007
T2 - 5th International Seminar on Aerospace Science and Technology, ISAST 2017
Y2 - 27 September 2017 through 29 September 2017
ER -