The delta wings in modern days large operated in jet fighter aircraft. The tremendous changes in the wing design of delta wing. Using 2-D and 3-D model analysis for different delta wing configuration will be analyzed Using ANSYS-FLUENT.
The simulation of different configuration will be carried out using k-Ω (SST) model for sonic, transonic, supersonic conditions.
The optimum performance carried out of different configuration to be analyzed & calculating wave drag by manual technique. Compare different delta wing configuration by graphs which plotted in Microsoft word.
The simulation of different configuration will be carried out using k-Ω (SST) model for sonic, transonic, supersonic conditions.
The optimum performance carried out of different configuration to be analyzed & calculating wave drag by manual technique. Compare different delta wing configuration by graphs which plotted in Microsoft word.
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