1 |
KDS 1520-4001, "Helicopter, Utility", Defense Acquisition Program Administration, 2013.
|
2 |
KDS 1620-4009, "Main Landing Gear, Fixed", Defense Acquisition Program Administration, 2013.
|
3 |
J. H. Choi, M. W. Chang, Y. W. Lee, J. J. Yoon, "An Improvement Study on Stick-Slip Behavior of Nose Landing Gear for Rotary Wing Aircraft", KSAA, Vol.25, No.3, pp.61-67, 2017. DOI : https://doi.org/10.12985/ksaa.2017.25.3.061
|
4 |
J. H. Choi, M. W. Chang, H. G. Lim, J. S. Lee, "A improvement Study on Safety Assurance of Main Landing Gear Failure for Rotary Wing Aircraft", J. of The Korean Society for Aeronautical and Space Sciences, Vol.45, No.6 pp.490-497, 2017. DOI : https://doi.org/10.5139/JKSAS.2017.45.6.490
DOI
|
5 |
B. H. Choi, "RB-FA-G003 Fracture Surface Analysis", Korea Research Institute of Standards and Science, 2011, Available from:https://www.randb.co.kr/wp-content (accessed Feb. 20,2019)
|
6 |
Abaqus User's Guide, Dassault Systems, 2014, Available from:https:/130.149.89.49:2080/v6.11/pdf_bo oks/CAE.pdf (accessed Jun. 1, 2019)
|
7 |
J. S. Przemieniecki, "Aircraft Landing Gear Design : Principles and Practices", AIAA Education Series, 1988. DOI : https://doi.org/10.2514/4.861468
|
8 |
James M. Gere, "Mechanics of Materials", Thomson Learning, Inc, 2004
|
9 |
Fatigue Basic Theory, CAIWARE, 2015, available from: https://caiware.com (accessed Feb. 5, 2018)
|
10 |
Goodman's Fatigue Equation, NFX MIDAS, 2013, Available from : https://kor.midasuser.com/nfx/techpaper/keyword_view.asp?idx=326 (accessed Dec. 5, 2018)
|
11 |
MIL-HDBK-5J, Federal Aviation Administration, "Metallic Materials and Elements for Aerospace Vehicle Structures", 2003
|
12 |
88PR6241, "Fatigue Test Report for KUH Main Landing Gear" Korea Aerospace Research Institute, 2010
|
13 |
MIL-A-83444, Federal Aviation Administration, "Airplane Damage Tolerance Requirements", 1974
|