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Advanced IR System For Supersonic Boundary Layer Transition Flight ExperimentInfrared thermography is a preferred method investigating transition in flight: a) Global and non-intrusive; b) Can also be used to visualize and characterize other fluid mechanic phenomena such as shock impingement, separation etc. F-15 based system was updated with new camera and digital video recorder to support high Reynolds number transition tests. Digital Recording improves image quality and analysis capability and allows for accurate quantitative (temperature) measurements and greater enhancement through image processing allows analysis of smaller scale phenomena.
Document ID
20080042408
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Banks, Daniel W. (NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 24, 2013
Publication Date
October 7, 2008
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: Fundamental Aeronautics Program Annual Meeting 2008
Location: Atlanta, GA
Country: United States
Start Date: October 7, 2008
End Date: October 9, 2008
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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