Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems.

Abstract

This part describes the results of a survey conducted to determine the present and the estimated 1970 capabilities of sensors applicable to the control of aircraft propulsion systems. The survey included electromechanical and fluid amplifier (fluidic) sensors for measurement of gas dynamic and static properties as well as for measurement of airframe dynamic parameters. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1968
Accession Number
AD0852757

Entities

People

  • Isaac A. Ogura
  • Ronald G. Wolfshagen

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Amplifiers
  • Cooperation
  • Engineering
  • Fluidic Amplifiers
  • Measurement
  • Propulsion Systems
  • Systems Engineering

Readers

  • Business Analytics
  • Electrical Engineering
  • Structural Dynamics.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems