In the transverse cross -section where the integrated flow was adjacent, the oval body and the environment were recognized as optimally with controlled wing. Such an element helps to create additional lifting force and improves the aerodynamic properties of the aircraft. At the same time, it increases the height of the building wing at the root, which allows you to increase its elongation – an important parameter to reduce air resistance.

The integral flow also provides an additional internal volume in which chassis and other aircraft systems can be placed. This solution not only improves the design, but also saves space and makes the plane more functional.

The oval and straightened body provides a decrease in the front resistance and provides you to rationally organize the interior. The passenger region will be located on the upper deck and the cargo compartment at the bottom. This layout provides an increase of approximately 45% in load compared to classical bikameral solutions.

Instead of the traditional “wing pipe” scheme, engineers choose the integral structures in which the boundary between the body and the wing is eroded. Such aircraft are often called “flying wings, because it is difficult to determine where the case is over and the wing begins.

According to calculations, these new layouts can increase aerodynamic indicators by 25-30% compared to the best modern aircraft.

Source: Ferra

Previous articleIntel hired former Apple and Google senior executives in order to “compensate” computers on 23 June 2025, 16:30
Next articleAlert Xiaomi about 6 critical mistakes in some of the most popular mobile phones: if this happens to you, update as soon as possible
I am a professional journalist and content creator with extensive experience writing for news websites. I currently work as an author at Gadget Onus, where I specialize in covering hot news topics. My written pieces have been published on some of the biggest media outlets around the world, including The Guardian and BBC News.

LEAVE A REPLY

Please enter your comment!
Please enter your name here