1. Boundary layer control for hypersonic airbreathing vehicles;Berry,2004
2. Scramjet engines: the first forty years;Curran;J. Propuls. Power,2001
3. Supersonic wind tunnel tests of a half-axisymmetric 12 deg-spike inlet to a rocket-based combined-cycle propulsion system;DeBonis,2001
4. Experimental investigation of starting process for a variable geometry air inlet operating from Mach 2 to Mach 8;Falempin,2006
5. Experimental investigation of a hypersonic inlet with and without sidewall compression;Gruhn;J. Propuls. Power,2011