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JA5 Canard Aircraft Aerodynamic Analysis

The images below depict results of aerodynamic analysis of the JA5. This aerodynamic analysis was used to calculate stability characteristics and aircraft performance and to generate loads models for structural analysis. This analysis was used iteratively during the design process to produce the final configuration.


Vortex Lattice Model of the JA5

Vortex Lattice AVL Model of the JA5 Walrus Aircraft

Trefftz Plot -- Cruise Condition

Trefftz Plot, Cruise Condition, JA5 Walrus Aircraft

Aicraft Modeled Using 3-D Panel Code

Aircraft Modeled Using 3-D Panel Code

Surface Pressure Plot - VSAero Panel Method

Surface Pressure Plot - VSAero Panel Method

Streamlines with Pressure Plot

Streamlines with Pressure Plot - VSAero Panel Method