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교과목의 개요
This course will provide a systematic approach to V/STOL aircraft. It will cover the following: development history of V/STOL aircraft, fundamental and conceptual theory of aerodynamics, estimation of power required, problems related to maintenance, prediction of performance for take-off and landing, and design of high lift and propulsion system. -
T.A
Balakumaran, Natarajan -
성적 평가 방법
Mid-term test(30%), Final exam(40%), Homework(20%), Attendance(10%) -
교재 및 참고서
Textbook/교과서
ALFRED GESSOW, GARRY C. MYERS JR, Aerodynamics of the Helicopter, 8th Printing 1985., College Park Press
References/참고서
Bramwell, A. R. S., Done, G T. S., and Balmford, D., "Helicopter Dynamics," Butterworth_Heinemann, 2001
Seddon, J. and Newman, S., "Basic Helicopter Aerodynamics," AIAA Education Series, 2001
Stepniewski, W. Z. and Keys, C. N., "Rotary Wing Aerodynamics," Dover Publications, 1984
Prouty, R. W., "Helicopter Perfomance, Stability, and Control," PWS Publications, 1986
서울대학교 지능형 공탄성 및 헬리콥터 연구실
서울특별시 관악구 관악로 1 서울대학교 기계항공공학부 지능형 공탄성 및 헬리콥터 연구실301동 1357호 전화 : 02-880-1901 (내선 1901) / 302동 213-1호 Tel: 02-880-1608 (내선 1608)
개인정보관리책임자 : 은원종 (eun0914@snu.ac.kr)
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