Optimization Efficiency of the Aircraft Wing of Cessna 172 Skyhawk by Absorbent Adverse Pressure Using Tangential Suction Slot Without Vacuum Device | Zendy

Naseer A. Mousa | Zendy; Osam H. Attia | Zendy; Hussein A. Mahmood | Zendy; Nor Mariah Adam | Zendy

Open Access

Optimization 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

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

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