Aqib Habib

• Utilized CATIA V5 for the design of vertical stabilizer, ground-control station and control surfaces for scaled-down high-performance aircraft • Utilized classical laminate theory and Puck's failure theory to design and develop CFRP control surfaces and fuselage skin. • Successfully designed and manufactured aircraft mockup model for scaled-down high-performance aircraft using laser cutting • Delivered manufacturing drawings with CATIA V5 and GD&T principles

•Designed and delivered a tilt-wing and tilt-rotor eVTOL UAV prototype •Utilized XFLR5, advanced aircraft analysis and MATLAB for the development of the project in the conceptual and preliminary design phase • Utilized solidworks for the design of aircraft loft, assemblies and parts • Designed CFRP fuselage, wings, and vertical stabilizer by utilizing CLT. • Utilized ANSYS Mechanical for the finite element analysis of motor mounts

•Delivered detailed HVAC load analysis model using MATLAB/Simscape •Reduced laboratory costs by $3000/month •Validated model results within the HVAC lab

• Designed and delivered a CFRP fixed-wing eVTOL UAV • Utilized solidworks for the design of aircraft loft, assemblies and parts • Designed CFRP fuselage, wings, horizontal and vertical stabilizer assembly by utilizing CLT • Utilized XFLR5, and MATLAB for the development of the project in the conceptual and preliminary design phase • Utilizing bench testing to measure the strength of additively manufactured motor mounts

Graduated as a Gold Medalist