Browse TRAIL Inventories

Investigation of a simple device for preventing separation due to shock and boundary-layer interaction

Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing

Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61

Factors affecting transition at supersonic speeds

Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05

Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles

Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine

Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶


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