A PRESSURE CONTROL SYSTEM FOR A HYPERSONIC WIND TUNNEL,

Abstract

Contents: Introduction; Test Facility, Details of the Air Storage System; Regenerative Gas Fired Heat Exchanger; Air Flow Control System; Air Control Valves; Hydraulic System; Servo Amplifier; Pressure Sensing Devices; Control Computer-Design considerations, Construction details, Modus operandi of the analogue control; Resume of Performance.

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1963
Accession Number
AD0426233

Entities

People

  • I. L. Smith
  • W. H. Horton

Organizations

  • Stanford University

Tags

DTIC Thesaurus Topics

  • Air Flow
  • Control Systems
  • Flow
  • Heat Exchangers
  • Hypersonic Wind Tunnels
  • Hypervelocity Flow
  • Research Facilities
  • Shock Tunnels
  • Test Facilities
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow