Accession Number:

AD0258468

Title:

THE THERMAL BARRIER IN SUPERSONIC FLIGHT (SELECTED PARTS)

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• ZHOVINSKIY,N. YE.

Report Date:

1961-02-01

Pagination or Media Count:

1.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE