Optimized Structure Design of Composite Cyclocopter Rotor System using RSM |
Hwang In Seong
(서울대학교 기계항공공학부)
Hwang Chang Sup (서울대학교 기계항공공학부) Kim Min Ki (서울대학교 기계항공공학부) Kim Seung Jo (서울대학교 기계항공공학부, 비행체특화연구센터) |
1 | Yun, C.Y., 'A New Vertical Take-off and Landing Aircraft with Cycloidal Blades System Cyclocopter,' Ph.D thesis, Seoul National University, 2004 |
2 | Hwang, I.S., Min, S.Y., Kim M.K. and Kim, S.J., 'Multidisciplinary Optimal Design of Cyclocopter Blade System,' 1st AlAA MDO Specialist Conference, Austin, TX, April 18-21, 2005 |
3 | Myers, R. H. and Montgomery, D.C. Response surface methodology process and product optimization using designed experiments, New York Wiley, 1995 |
4 | Jones, R.M. Mechanics of composite materials, 2nd Edition, Taylor & Francis, 1999 |
5 | Wheatley, J.B 'Simplified Aerodynamic Analysis of the Cyclogiro Rotating-wing System,' Technical Notes NACA, No. 467, August 1933 |
6 | Gen, M. and Cheng, R. Genetic algorithms and engineering optimization, New York Wiley, 2000 |
7 | Kirsten, F.K. 'Cycloidal propulsion in air,' Bulletin No. 79, Engineering Experiment Station Series, University of Washington, March 1935 |
8 | Gibbens, R.P. and Boschma, J.H. 'Construction and testing of a new aircraft cycloidal propeller,' 13th AlAA Lighter-Than-Air Systems Technology conference, Norfolk, VA, June 28-July 1, AIAA No. 99-3906, pp. 1-9, 1999 |