8/20/2023 0 Comments X wing front viewEach tank occupies the space between the leading edge and trailing edge high-lift structure and associated mechanisms. Such factors must be considered separately when deciding the overall location of fuel tanks.įor the aircraft in this project, we can consider the fuel to be held in wing tanks on each side of the aircraft fuselage as shown in Figure 4.7. Note: these factors do not account for landing gear or other significant intrusions into the available space. Typically, reduce the available internal volume to 85 per cent for integral tanks and to 65 per cent for bladder or ‘bag tanks’. To determine the usable capacity of a fuel tank it is possible to calculate the external volume and then reduce this value to account for internal obstructions caused by structural and system components within the tank. Marchman III, in Aircraft Design Projects, 2003 Estimation of wing fuel volume
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |