FEASIBILITY STUDY OF CRITICAL PART COOLING AND CLOSED LOOP CONTROL FOR AIRCRAFT ELECTRONIC COOLING SYSTEMS (FORCED AIR TYPE).

Abstract

This report presents the results of a program of analysis and testing to determine the feasibility of applying closed loop control system methods to cooling systems for aircraft electronics.

Document Details

Document Type
Technical Report
Publication Date
Sep 21, 1967
Accession Number
AD0834679

Entities

People

  • A. R. Saltzman
  • B. T. Plizak
  • L. F. Tomko

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Control Systems
  • Feasibility Studies

Readers

  • Combustion and Flow Dynamics.
  • Software Engineering

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems