ORCID as entered in ROS

Select Publications
2016, Validation of DST Group’s HIFiRE-4 Glider Aerodynamic Database via Hypersonic Free-Flight: Final Report, DST Group, 1
,2014, Leading-Edge Separation in Thermal Nonequilibrium Hypersonic Flow, US Air Force Asian Office of Aerospace Research and Development, AOARD-134013
,2005, Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers, US Air Force Office of Space Research Report AOARD-02-4001, A981934
,