Subsonic Choked Flow LDV Calibrator/Velocity Standard Development

Abstract

In an LDV entry in the AEDC 1-Ft Transonic Wind Tunnel where harsh environmental conditions exist; e.g., high temperature, vibration, etc., an asymptotic drift in measured flow velocity of a few percent was noticed following startup each day. To resolve the issue of whether the tunnel or the LDV was responsible and to aid in the correction of the problem, a device was developed which produces invariant particle velocities for use as a velocity standard in the tunnel environment. The development of such a device is herein discussed. The analysis demonstrates the device to be satisfactory for resolution of the "startup drift" problem and, with some additional development, could be used in checkout and calibration of an LDV.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1985
Accession Number
ADA539257

Entities

People

  • Peter M. Sherrouse

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Supplies
  • Boundary Layer
  • Control Systems
  • Flow
  • Flow Fields
  • Fluid Flow
  • Governments
  • High Temperature
  • Mach Number
  • Measurement
  • Nozzles
  • Standards
  • Subsonic Nozzles
  • Temperature Gradients
  • Velocimeters
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.