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Developments in flow visualization methods for flight researchWith the introduction of modern airplanes utilizing laminar flow, flow visualization has become an important diagnostic tool in determining aerodynamic characteristics such as surface flow direction and boundary-layer state. A refinement of the sublimating chemical technique has been developed to define both the boundary-layer transition location and the transition mode. In response to the need for flow visualization at subsonic and transonic speeds and altitudes above 20,000 feet, the liquid crystal technique has been developed. A third flow visualization technique that has been used is infrared imaging, which offers non-intrusive testing over a wide range of test conditions. A review of these flow visualization methods and recent flight results is presented for a variety of modern aircraft and flight conditions.
Document ID
19910071121
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holmes, Bruce J.
(NASA Langley Research Center Hampton, VA, United States)
Obara, Clifford J.
(NASA Langley Research Center Hampton, VA, United States)
Manuel, Gregory S.
(NASA Langley Research Center Hampton, VA, United States)
Lee, Cynthia C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Instrumentation
Meeting Information
Meeting: International Symposium
Location: Prague
Country: Czechoslovakia
Start Date: August 21, 1989
End Date: August 25, 1989
Accession Number
91A55744
Distribution Limits
Public
Copyright
Other

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