The phrase "aircraft section" is correct and usable in written English.
It can be used to refer to a specific part or division of an aircraft, often in technical or engineering contexts.
Example: "The aircraft section responsible for the wings must ensure structural integrity during flight tests."
Alternatives: "aircraft component" or "aircraft division".
This investigation has applied a computational fluid dynamics (CFD) program to model a two-dimensional aircraft section insulated by such an air channel.
In the Operations notes, Formation Flying, orders specifically stated that the formation, as a whole, was not to stay together, saying each six aircraft section was to be a self-contained defensive unit, flying at different heights, stating that more than 12 aircraft per formation made it unwieldy and unmanageable by one leader.
The work being done in Mobile involves just the final assembly of aircraft sections that will continue to be built in Europe.
ASI sells some aircraft sections to flight training schools and others to the entertainment industry for movies like "World War Z," "Johnny English" and the "Batman" and "Star Wars" franchises.
The staff at GQG had the use of a detachment of the 8th Engineer Regiment, a company of the 19th Railway Squadron, two companies of the 68th Territorial Infantry Regiment, a company of Forestry Chasseurs, two anti-aircraft sections, up to two carrier pigeon units, a unit of cyclist messengers, a medical detachment and a military police escort squadron.
The research activity focuses on the modelling and testing of a composite panel representing a local segment of an aircraft wing section, investigating in particular the buckling behavior under dynamic loading.
It also should be noted that the aircraft costing section is based on a segment approach, with aircraft acquisition, operating and crew costs, and some direct sales costs, as well as revenues, apportioned on a "segment" basis.
This far-field transmission study was conducted in a wide-body mock aircraft cabin section under ambient pressure and representative flight ventilation conditions.
First, the total number of particles at steady-state (row b) was divided by the total volume of air in the four-row aircraft cabin section, which was 26.9 m3.
In particular, to determine optimal sensor placement in a mock wide-body aircraft cabin section, CFD simulations have been used to model different chemical release conditions (continuous or discrete doses) and release rates (10−7, 10−6, or 10−5 m3/s [19], [19]).
From this aircraft, several sections or panels in different regions such as wing, vertical tailplane and fuselage are defined.
