Search U.S. government technical reports digitized or harvested by TRAIL.
Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane
Tests of Thermal-Electric De-Icing Equipment for Propellers
Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane With a Triangular Wing
Heat-transfer and boundary-layer transition on a heated 20 degree cone at a Mach number of 1.53