THE THERMAL BARRIER IN SUPERSONIC FLIGHT (SELECTED PARTS)

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

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1961
Accession Number
AD0258468

Entities

People

  • N. Ye. Zhovinskiy

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Carbides
  • Chemical Compounds
  • Compound Semiconductors
  • Electronics
  • Flight
  • Inorganic Carbon Compounds
  • Inorganic Chemicals
  • Mechanical Structure
  • Semiconductors
  • Solid State Electronics
  • Supersonic Flight
  • Titanium
  • Vibration

Readers

  • Combustion and Flow Dynamics.
  • Reinforced Composite Materials
  • Semiconductor Device Technology

Technology Areas

  • Hypersonics
  • Microelectronics
  • Microelectronics - Microelectromechanical Systems