1. Stivers, L. S. "Calculated Pressure Distributions and Components of Total-Drag Coefficients for 18 Constant-Volume, Slender Bodies of Revolution at Zero Incidence for Mach Numbers From 2.0 to 12.0, With Experimental Aerodynamic Characteristics for Three of the Bodies," , No. October, 1971.
2. Computational study of support influence on base flow of a model in supersonic flow
3. Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel on Hypersonic Boundary-Layer Transition
4. Chynoweth, B. C. "Measurements of Transition Dominated by the Second-Mode Instability at Mach 6," Ph.D. thesis,Purdue University, 2018. Issue: May.