Open AccessOptimization Efficiency of the Aircraft Wing of Cessna 172 Skyhawk by Absorbent Adverse Pressure Using Tangential Suction Slot Without Vacuum Device
Author(s) -
Naseer A. Mousa,
Osam H. Attia,
Hussein A. Mahmood,
Nor Mariah Adam
Publication year - 2022
Publication title -
mathematical modelling and engineering problems/mathematical modelling of engineering problems
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.26
H-Index - 11
eISSN - 2369-0747
pISSN - 2369-0739
DOI - 10.18280/mmep.090320
Subject(s) - wing , angle of attack , backflow , adverse pressure gradient , stall (fluid mechanics) , mechanics , drag , leading edge , static pressure , suction , lift (data mining) , materials science , wingtip vortices , flow separation , turbulence , structural engineering , aerodynamics , physics , vortex , engineering , inlet , horseshoe vortex , mechanical engineering , vorticity , meteorology , computer science , data mining