5-2 Experimental Investigations of the Flow Field around a Generic Re-entry Capsule in HIEST
Aerothermodynamic Flow Field Characteristics of Large Angle Blunt Cones at Mach 5.75
AIAA-2006-6347 Are Phase and Time-Delay Margins Always Adversely Affected by High-Gain?
Heat Transfer Measurements On Waverider at Hypersonic Mach Numbers (AIAA 2014-2507)
Transonic Airfoil Analysis by Explicit TVD Formulations of the Navier-Stokes Equations