01.1 - Aircraft Design and Integrated System (Basics and Theory)
THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE
L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network Institute of Aviation, Poland; ¹Military University of Technology, Poland
In the following paper the basic design assumptions of a new generation light combat airplane have been presented. What is more, the results of the aerodynamic characteristics identification process of the newly designed object were presented. Aerodynamic analysis was performed using specialized software based on solving partial differential equations using the Finite Volumes Method.