A Study of Develop Optical Instrumentation for the AFFDL Rent Facility

Abstract

The "RENT" facility is a high-enthalpy reentry nosetip test facility which employs a 50 megawatt arc heater to produce a high energy supersonic free jet test flow. The objectives of such tests include the determination of materials' response to simulated reentry conditions, heat transfer, erosion and ablation, and other aerodynamic effects. To attain the full utility of the facility requires both computation and measurement of the conditions and aerodynamic phenomena which occur during tests. The flow is in many respects too complex to allow accurate computation of all phenomena of interest. Therefore, measurements are needed to provide more accurate descriptions of many basic properties and phenomena. A number of optical measurement techniques have been attempted in the "RENT" facility with some degrees of success, and pro- grams to refine such methods have been active for several years. A study has begun recently to continue the development and application of optical diagnostic methods for this facility. The objective of this study is to examine candidate optical measurement techniques, to plan the development of such methods, and ultimately to apply developed techniques during actual test operations.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1978
Accession Number
ADA379795

Entities

People

  • A. G. Stringer
  • D. M. Parobek
  • J. D. Trolinger

Organizations

  • Flight Dynamics Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Cameras
  • Diffraction
  • Doppler Effect
  • Engineering
  • Flow Visualization
  • Heat Transfer
  • Helium Neon Lasers
  • Measurement
  • Optics
  • Particle Size
  • Photographic Materials
  • Photographs
  • Photography
  • Production Engineering
  • Surface Properties
  • Surface Roughness

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Mechanics and Fluid Dynamics.
  • Software Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow