1. Sanders, B.W. and Weir, L.J., “Aerodynamic Design of a Dual-Flow Mach 7 Hypersonic Inlet System for a Turbine-Based Combined-Cycle Hypersonic Propulsion,” NASA CR-215214, 2008.
2. Slater, J.W. and Saunders, J.D., “Computational Fluid Dynamics (CFD) Simulation of Hypersonic Turbine-Based Combined-Cycle (TBCC) Inlet Mode Transition,” 16th International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, AIAA 2009-7349, Oct. 2009.
3. Vance, F.D.III, “Computational Analyses of the LIMX TBCC Inlet High-Speed Flowpath,” NASA TM-217219, 2012.
4. Boundary-Layer Control in Mach 4 and Mach 6 Scramjet Engines
5. Effects of boundary-layers bleeding on unstart/restart characteristics of hypersonic inlets