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


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