The NASA High Lift Common Research Model (HL-CRM) is an aerodynamic research aircraft configuration developed by NASA. It serves as a versatile platform for studying high-lift systems and advanced aerodynamic technologies. The HL-CRM features a scaled-down, simplified version of a commercial transport wing with high-lift devices, such as flaps and slats, for enhanced lift and control during takeoff and landing. Its purpose is to investigate and optimize aerodynamic performance, efficiency, and safety in future aircraft designs, ultimately benefiting the aviation industry as a whole. In this project NASA HL-CRM Aircraft CAD Model is attached for CFD Study. Source of NASA HL-CRM Aircraft CAD Model is NASA: https://hiliftpw.larc.nasa.gov/Workshop4/geometries.html

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