Accession Number : AD0258468

Title :   THE THERMAL BARRIER IN SUPERSONIC FLIGHT (SELECTED PARTS)

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : ZHOVINSKIY,N. YE.

Report Date : FEB 1961

Pagination or Media Count : 1

Abstract : Contents: The thermal barrier Titanium and its alloys Protection of aircraft structures against over heating at high speeds Cooling Evaporative cooling Fuel cooling Cooling by ultrasonic vibrations Cooling by means of semiconductors

Descriptors :   *AERODYNAMIC HEATING, ABLATION, AIRCRAFT, AIRFRAMES, COOLING, HEAT EXCHANGERS, HEAT TRANSFER, JET FIGHTERS, MODEL TESTS, SEMICONDUCTORS, SUPERSONIC FLOW, SWEAT COOLING, THERMAL STRESSES, TITANIUM ALLOYS, ULTRASONIC RADIATION

Distribution Statement : APPROVED FOR PUBLIC RELEASE