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Investigation of the Flow Around an Aircraft Wing of Section NACA 2412 Utilising ANSYS Fluent
Rob Ives
, Stewart Keir
, Edet Bassey
,
Faik Hamad
SCEDT Engineering
Teesside University
Research output
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peer-review
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Keyphrases
ANSYS Fluent
100%
Flow around
100%
NACA 2412
100%
Aircraft Wing
100%
External Flow
100%
Three-dimensional (3D)
50%
Aerofoil
50%
Finite Aspect Ratio
50%
Aspect Ratio
50%
Low Velocity
25%
High Velocity
25%
Simulation Model
25%
Flow Condition
25%
Accurate Simulation
25%
Lift Curve Slope
25%
Stall
25%
Commercial Aircraft
25%
Aerodynamic Characteristics
25%
Wingtip
25%
Wing Geometry
25%
Root Tip
25%
Detailed Methodology
25%
Characteristic Difference
25%
Flow Physics
25%
Engineering
Wings
100%
External Flow
100%
Aspect Ratio
100%
Airfoil
50%
Simulated Data
25%
Simulation Model
25%
Flow Condition
25%
Characteristic Difference
25%
Flow Physic
25%
Commercial Aircraft
25%
Aerodynamic Characteristic
25%
Lift-Curve Slope
25%