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Design of Thermally Efficient Cryogenic Tanks for Spacecraft

Novel Mobility Solutions for Extreme Lunar Terrain

Design, Analysis and Testing of Ionic Wind Propulsion System for an Electric Aircraft

Structural Analysis and Design of the Aircraft Wing

Structural Design Analysis of the Burnelli CBY-3 Loadmaster and DC-3

Design of Thermally Efficient Cryogenic Tanks for Spacecraft

Micro-Aircraft Design for 2022 SAE AeroDesign Competition

Design and Testing of Lattice Structures for Noise Reduction

Estimation of a Plume with a UTV

Design, Implementation, and Testing of Apparatus to Investigate Combustion Phenomena R...