Title :
The effects of unsteady flow on aerodynamic characteristics of a tactical airplane´s wing
Author :
Svoboda, Ales ; Rozehnal, Dalibor
Author_Institution :
Univ. of Defence, Brno, Czech Republic
Abstract :
This paper provides an insight into the unsteady aerodynamic phenomena related to real-world applications, especially with regard to tactical aircraft. The physical model of unsteady flows and related processes is described, followed by a description of its impact on airplane applications. Further, a description of a wind tunnel experiment is given.
Keywords :
aerodynamics; aerospace components; aircraft; wind tunnels; airplane applications; tactical aircraft; tactical airplane wing aerodynamic characteristics; unsteady aerodynamic phenomena; unsteady flow effect; wind tunnel experiment; Aerodynamics; Airplanes; Atmospheric modeling; Automotive components; Electric breakdown; Hysteresis; aerodynamics; aircraft; airplane; flow; tactical; unsteady; vortex;
Conference_Titel :
Military Technologies (ICMT), 2015 International Conference on
Conference_Location :
Brno
Print_ISBN :
978-8-0723-1976-3
DOI :
10.1109/MILTECHS.2015.7153724
