항공기 설계 프로젝트 - Europa XS-Monowheel

소개

항공기 설계 프로젝트(A+)_Europa XS-Monowheel 자료 입니다.

설계 툴을 이용하여 Europa XS-Monowheel 을 타겟설계 해보았습니다.

목차

1. 서론
1)Europa XS-monowheel 형상
2)Europa XS-monowheel 제원

2. 본론
1)중량 추정
2)비행 성능
3)날개 및 플랩 설계
4)무게 중심
5)꼬리 날개

3. 결론
1)오차분석
2)고찰

4. 참고 문헌

본문내용

2) Europa XS-monowheel 제원

Model name
Europa XS Monowheel
Engine
Rotax 912 ULS
Wing
27.133 ft
Aspect Ratio
7.096
Overall length
19.17 ft
Overall height
4.33 ft
Baggage space
22.50
Maximum take-off weight
1370 lb
Empty weight
835 lb
Maximum baggage capacity
80 lb
Wing loading at max take-off weight
13.42 lb/
Power loading
13.7 lb/hp
Stall speed flaps extended
44 kts
Stall speed clean
52 kts
Cruise speed 8,000 ft 75 % pwr
(Rotax 912 ULS)
135 kts
VNE (IAS)
165 kts
Take-off ground roll at gross weight
590 ft
Landing roll
600 ft
Rate of climb at 1370 lb gross weight
1000 fpm
Maximum Fuel
15 imp gal / 68 liter
Fuel consumption
3,14 imp gal/hr
Standard Tank Range at 75% power
732 nmile
Power
100hp
Wing root chord
50 inch
Wing tip cord
40 inch
Taiplaine span
8 ft
Tailplane area
22
Fuselage width
44 inch
Fuselage / Wing Xcg
7.08 / 4.48 ft
tip/root wing air foil
dykins 12% / dykins 12%
Wing area
100
Ailerons (total) area
6.65

참고자료

· http://www.europa-aircraft.com/monowheel/specification.php
· http://www.europa-aircraft.com/
· Europa XS-monowheel manual
· http://www.europa-aircraft.co.uk/upload/xs_mw_owners_manual.pdf
· 비행역학, 윤용현 지음, 경문사, 2008
· 항공기 개념설계, 항공기설계교육연구회, 경문사, 2010