Impact of Varying Wall Temperature on Hypersonic Boundary Layers
Undergraduate research at Purdue’s Aerospace Sciences Laboratory on how varying wall temperature affects hypersonic boundary layers. Completed and presented a sharp cone transition study; now extending the work to a flared cone, pairing STABL computations with BAM6QT wind tunnel experiments.
Tools: STABL, DPLR2D, PSE-Chem, MATLAB, Tecplot
