Calibration and Validation Studies in the LENS Facility

Abstract

This report describes recent developments in the LENS facility, flow field calibration studies, and aerothermal and aero-optical measurements to evaluate the turbulent flow field characteristics of seeker head configurations in hypervelocity airflow. The development of the LENS facility to run at pressure levels up to 30,000 psi and temperatures up to 14,000 deg R are reviewed. Issues associated with diaphragm performance, reservoir configuration, throat melting and burning, and modifications to the facility for large recoil loads at high pressure operation are briefly reviewed. Flow field measurements made during calibration studies are compared with computer predictions. Validation studies with simple seeker head aperture configurations in high enthalpy flows are then discussed. The models and aerothermal and aero-optical instrumentation used in these studies are described. The measurements obtained in flows up to 12,000 ft/sec are compared with similar measurements at lower velocities, simple correlation techniques, and detailed computer simulations.

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Document Details

Document Type
Technical Report
Publication Date
Feb 09, 1994
Accession Number
ADA278403

Entities

People

  • Michael Holden

Organizations

  • Calspan-University of Buffalo Research Center

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Data Processing
  • Detectors
  • Distortion
  • Flow Fields
  • Infrared Detectors
  • Laser Beams
  • Laser Induced Fluorescence
  • Lasers
  • Measurement
  • Shock Tunnels
  • Test And Evaluation
  • Test Facilities
  • Three Dimensional
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Astronomy and Astrophysics.
  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow