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Variable-Sweep Transition Flight Experiment (VSTFE): Stability code development and clean-up glove data analysisThe primary objective of the Variable Sweep Transition Flight Experiment (VSTFE) was to establish an improved swept wing transition criterion. The development of the Unified Stability System gave a way of quickly examining disturbance growth for a wide variety of laminar boundary layers. The disturbance growth traces shown are too scattered to define a transition criteria to replace the F-111 data band, which has been used successfully to design NLF gloves. Still, a careful review of the clean-up glove data may yield cases for which the transition location is known more accurately. Liquid crystal photographs of the clean-up glove show much spanwise variation in the transition front for some conditions, and this further complicates the analyses. Several high quality cases are needed in which the transition front is well defined and at a relatively constant chordwise station.
Document ID
19900003232
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rozendaal, Roger A.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Publication Information
Publication: NASA, Langley Research Center, Research in Natural Laminar Flow and Laminar-Flow Control, Part 3
Subject Category
Aircraft Design, Testing And Performance
Accession Number
90N12548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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