Method of formalizing the layout of the internal compartments of aircraft
Journal Title: INCAS BULLETIN - Year 2019, Vol 11, Issue 0
Abstract
The mathematical formulation of the aircraft’s internal layout problem is described as an optimization problem, with an indication of its objective function, constraints, and performance criteria. The approach (receptor methods and apparatus of normal equations) is justified, which makes it possible to move from enumeration method of placing added objects to intelligent algorithms of automated placement when creating geometric models of automated layout. It was shown that preparing the aircraft for layout automation complicates the mathematical description of geometric models of added objects, increases the complexity of their visualization in modern computer graphics systems and makes the need to create an additional interface between new geometric models and common CAD systems (SolidWorks, AutoCAD, COMPAS, etc.).
Authors and Affiliations
Mikhail Yu. KUPRIKOV, Leonid V. MARKIN
Keywords
Related Articles
- EP ID EP612831
- DOI 10.13111/2066-8201.2019.11.S.14
- Views 83
- Downloads 0
Optimization study of using PTC for human body heating dissipation
A better knowledge of the human body heat loses mechanisms is important for both diminishing the number of deaths during the surgical procedures of the patients under effect of full anaesthesia and increasing the efficie...
A Linear Analysis of a Blended Wing Body (BWB)Aircraft Model
In this article a linear analysis of a Blended Wing Body (BWB) aircraft model is performed. The BWB concept is in the attention of both military and civil sectors for the fact that has reduced radar signature (in the abs...
[b]Henri Coanda, a visionary in science and technology[/b]
Loads in the design of flight vehicles
The calculation of flight loads is a critical part of air vehicle design. On the other hand, the prediction of accurate loads is a sophisticated and complex process that requires skilled and experienced engineers. They m...
A 2D description of the single crystal thin plate growth from the melt by micro- pulling- down method. Part 2
This paper is the second part of a 2D description of a single crystal thin plate growth by micro-pulling–down (μ-PD) method. This part concerns the following aspects: temperature distribution and melt flow in the melt–cr...