Reconstruction of a Three-Dimensional Transonic Rotor Flow Field from Holographical Interferogram Data.

Abstract

Holographic interferometry and computer-assisted tomography (CAT) are used to determine the transonic velocity field of a model rotor blade in hover. A pulsed ruby laser recorded 40 interferograms with a 2-ft-diam view field near the model rotor-blade tip operating at a tip Mach number of 0.90. After digitizing the interferograms and extracting fringe-order functions, the data are transferred to a CAT code. The CAT code then calculates the perturbation velocity in several planes above the blade surfaces. The values from the holography-CAT method compare favorably with previously obtained numerical computations in most locations near the blade tip. The results demonstrate the technique's potential for three-dimensional transonic rotor flow studies.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1985
Accession Number
ADA152617

Entities

People

  • F. Becker
  • J. K. Kittleson
  • Y. H. Yu

Organizations

  • Ames Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Birds
  • Blade Tips
  • Cameras
  • Emulsions
  • Flow Fields
  • Helicopter Rotors
  • Helicopters
  • Laser Beams
  • Mach Number
  • Photographic Film
  • Photographs
  • Photography
  • Refractive Index
  • Three Dimensional
  • Three Dimensional Flow
  • Transonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Image Processing and Computer Vision.

Technology Areas

  • Directed Energy