Mathematical Modeling of the AEDC (Arnold Engineering Development Center) Propulsion Wind Tunnel (16T)

Abstract

An empirically based model of the 16-ft transonic Wind Tunnel (16T) in the Propulsion Wind Tunnel Facility at the Arnold Engineering Development Center, has been developed for calculating the distribution of tunnel component pressure losses and the effect of changes in these pressure losses on the tunnel total-power requirements. The model consists of two separate computer programs. The Historical Program assesses tunnel performance from a historical data base which was acquired during prior tunnel operation. The Analytical Model uses component pressure-loss information calculated by the Historical Program to evaluate potential changes in tunnel component pressure losses with respect to the tunnel power. The model was used to assess the potential power savings for a modification to the Tunnel 16T diffuser which involves the replacement of the compressor protective screen. Results indicate that for each 1-percent increase in diffuser recovery, a 4-percent decrease in main drive power will result. Less significant power savings were found for improvements to the other tunnel components. Additional keywords: Flow equations, Thermodynamics, Computations.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1985
Accession Number
ADA151293

Entities

People

  • P. B. Stich

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Barometric Pressure
  • Classification
  • Coefficients
  • Compressors
  • Computer Programs
  • Computers
  • Data Sets
  • Dynamic Pressure
  • Energy Consumption
  • Engineering
  • Equations
  • Static Pressure
  • Test Facilities
  • Transonic Wind Tunnels
  • United States
  • Wind Tunnels

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.
  • Aerospace Engineering