1. Mach 8 to 22 studies of flow separations due to deflected control surfaces
2. An investigation of flow separation and aerodynamic controls at hypersonic speeds.
3. Holden, M.S. "Separated Flow Studies at Hypersonic Speeds, Part 11:Two-dimensional Wedge Separated Flow Studies,"AF-1285-A-13 (2),December 1964.
4. Holden, M.S. "Theoretical and Experimental Studies of Laminar Flow Separation on Flat Plate-Wedge CompressionSurfacesin theHypersonicStrongInteraction Regime,"ARL 67-0112,May 1967.