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Holographic flow visualization at NASA LangleyHolographic flow visualization systems at two NASA Langley facilities, a hypersonic blow-down tunnel using CF4 gas and an expansion tube with very short test time, are described. A pulsed ruby laser is used at a CF4 tunnel for single pulse holography, double pulse with several minutes between exposures, and dual plate holographic interferometry. Shadowgraph, schlieren, and interferograms are reconstructed from the holograms in a separate reconstruction lab. At the expansion tube the short run time of 200 microseconds requires precise triggering of its double pulsed ruby laser. With double pulse capability of 20 to 1200 microseconds pulse separation, one pulse can occur before and one later after flow is established to obtain fringe free background interferograms (perfect infinite fringe) or both pulses can occur during flow in order to study flow instabilities. Holograms are reconstructed at the expansion tube with an in-place setup which makes use of a high power CW Argon laser and common optics for both recording and reconstructing the holograms. The holographic systems at the CF4 tunnel and expansion tube are operated routinely for flow visualization by tunnel technicians. Typical flow visualization photographs from both facilities are presented.
Document ID
19800028465
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Burner, A. W.
(NASA Langley Research Center Hampton, VA, United States)
Goad, W. K.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: International Instrumentation Symposium
Location: Anaheim, CA
Start Date: May 7, 1979
End Date: May 10, 1979
Sponsors: ISA
Accession Number
80A12635
Distribution Limits
Public
Copyright
Other

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