Expected Productivity Benefits Resulting from the New Data Acquisition, Processing, and Control System for Tunnel 16T at AEDC

Abstract

Requirements for large scale transonic wind tunnel test capability into the next century necessitate that significant sustainment efforts be undertaken for U.S. facilities to maintain reliable and efficient testing services. Many national facilities located at the major NASA centers and the Department of Defense's Arnold Engineering Development Center (AEDC) are in the middle of or preparing for major refurbishment programs. In Fiscal Year 1998, the Propulsion Wind Tunnel (PWT) Facility at AEDC launched a 7 year, $80M sustainment program which will improve reliability, reduce testing cycle time, reduce the number of operational station keepers, and improve the quality of test data in the 16 foot transonic and supersonic wind tunnels. A major part of this program is a total replacement of the data acquisition, processing and control systems in Tunnel 16T. This effort will provide major improvements in productivity of the test process as well as improved reliability and quality of data. This effort, along with ongoing maintenance and improvement projects, will sustain the world class status of this important development wind tunnel.

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Document Details

Document Type
Technical Report
Publication Date
Jun 18, 1998
Accession Number
ADA371002

Entities

People

  • David Rollins
  • Dennis Rose
  • Philip Stich

Organizations

  • American Institute of Aeronautics and Astronautics

Tags

Communities of Interest

  • Biomedical
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Acquisition
  • Control Panels
  • Control Systems
  • Data Acquisition
  • Data Processing
  • Data Reduction
  • Data Transmission
  • Digital Data
  • Engineering
  • Instrumentation
  • Local Area Networks
  • Measurement
  • Network Protocols
  • Software Development
  • Steady State
  • Strain Gages
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow