Stagnation and Dynamic Pressure Limits for the S1 Wind Tunnel

Abstract

The ARL-Salisbury S1 wind tunnel is a closed circuit, continuous, variable pressure wind tunnel, with a Mach number range of 0.35 to 1.0 and 1.4 to 2.8. The nominal dimensions of the tunnel's working section are 380 mm x 380 mm. Although the tunnel has been in operation for many years, no attempt has been made to experimentally investigate and establish the operational pressure limits. Thus, it is not uncommon for new experimenters to request running conditions which tunnel cannot achieve. This is further complicated by new temperature and current limits being adopted in 1985 after a main monitor failure. Therefore, a series of wind tunnel test runs were carried out in order to provide a reliable guide, outlining the running conditions which the S1 wind tunnel can safely achieve. This report outlines the absolute maximum pressure and the recommended maximum operating pressures for the S1 wind tunnel. The pressure limits calculated in this report were obtained from actual wind tunnel data records.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1991
Accession Number
ADA242989

Entities

People

  • David A. Pierens

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Temperature
  • Department Of Defense
  • Dynamic Pressure
  • Electrolytes
  • Equations
  • Flow
  • Mach Number
  • Measurement
  • Mechanics
  • Reynolds Number
  • Stagnation Pressure
  • Stagnation Temperature
  • Static Pressure
  • Variable Pressure
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Engineering

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Electronics Engineering
  • Software Engineering