Browse TRAIL Inventories

Boundary-layer transition on a cooled 20 degree cone at Mach numbers of 1.5 and 2.0

Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02

Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52

Lateral-Control Characteristics and Dihedral Effect of a Wing-Body Combination With a Variable-Incidence Triangular Wing and Wing-Tip Ailerons at a Mach Number of 1.52

Lateral Control Characteristics and Dihedral Effect of a Wing-Body Combination With a Variable Incidence Triangular Wing and Wing-Tip Ailerons at a Mach Number of 1.52

Preliminary investigation of a variable-area auxiliary air-intake system at Mach numbers from 0 to 1.3

Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44

Preliminary Investigation of a Family of Diffusers Designed for Near Sonic Inlet Velocities

Investigation of the Performance and Internal Flow of a Variable-Area, Variable-Internal-Contraction Inlet at Mach Numbers of 2.00, 2.50, and 2.92

Viscous Flows in Inlets


Published Year

Author