Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind TunnelsThomas Horvath, Chau-Lyan Chang, Brian R. Hollis et al.|32nd AIAA Fluid Dynamics Conference and Exhibit|2002Cited by 153
Boundary Layer Control for Hypersonic Airbreathing VehiclesScott Berry, Thomas Horvath, Robert Nowak|34th AIAA Fluid Dynamics Conference and Exhibit|2004Cited by 49
Discrete Roughness Transition for Hypersonic Flight VehiclesScott Berry, Thomas Horvath|45th AIAA Aerospace Sciences Meeting and Exhibit|2007Cited by 33
Comparison of Methods for Determining Boundary Layer Edge Conditions for Transition CorrelationsDerek S. Liechty, Thomas Horvath, Scott Berry et al.|33rd AIAA Fluid Dynamics Conference and Exhibit|2003Cited by 25
Assessment and Mission Planning Capability for Quantitative Aerothermodynamic Flight Measurements Using Remote ImagingThomas Horvath, Bill Wood, Scott Splinter et al.|Unknown|2008Cited by 22