Browse TRAIL Inventories

Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane

An analytical investigation of thermal-electric means of preventing ice formations on a propeller blade

Tests of Thermal-Electric De-Icing Equipment for Propellers

An Investigation of the Characteristics of Alcohol-Distribution Tubes Used for Ice Protection on Aircraft Windshields

The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight

The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight

Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane With a Triangular Wing

Comparison of Theoretical and Experimental Heat-Transfer Characteristics of Bodies of Revolution at Supersonic Speeds

Heat-transfer and boundary-layer transition on a heated 20 degree cone at a Mach number of 1.53

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


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