전문 번역가, 번역 회사, 웹 페이지 및 자유롭게 사용할 수 있는 번역 저장소 등을 활용합니다.
the maximum variation of toe-settings and camber angle for the test position shall be within ± 0,5 ° with maximum vertical load.
največje odstopanje stekanja in previsnega kota na preskusnem položaju pri maksimalni navpični obremenitvi je v območju ± 0,5°.
a diagram no 2, being a transverse cross section of the tanks showing, in particular, the radius of the bilge, the camber, the height of the trunk and the method of construction of the guiding device.
diagram št. 2, ki je prečni presek cistern in kaže zlasti polmer boka, izbočenost, višino debla in način konstrukcije vodila.
==variable-sweep aircraft=====experimental===*westland-hill pterodactyl iv* bell x-5* dassault mirage g* messerschmitt me p.1101* grumman xf10f-1 jaguar===production===* general dynamics f-111 aardvark* grumman f-14 tomcat* mikoyan-gurevich mig-23* mikoyan-gurevich mig-27* panavia tornado* rockwell b-1 lancer* sukhoi su-17* sukhoi su-24* tupolev tu-22m* tupolev tu-160==see also==* adaptive compliant wing* oblique wing* variable-incidence wing* variable camber wing==references==
variable-sweep wing ali "swing wing")", tudi krilo s spremenljvo geometrijo (spremenljivo puščico) je krilo, ki lahko v letu spreminja naklon.