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Development of a system for transition characterizationThe present system for real-time boundary layer transition detection and characterization encompasses aerodynamic simulations, sensor characteristics, and a hybrid analog/digital system for signal analysis, verification, and compression. By using artificial, intermittently laminar/turbulent signals, in conjunction with trajectory simulation, it becomes possible to conduct algorithm development which is independent of, and in advance of, sensor buildup. Attention is given to the illustrative case of the Pegasus launch vehicle's trajectory.
Document ID
19930063249
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bertelrud, Arild
(NASA Langley Research Center Hampton, VA, United States)
Graves, Sharon
(NASA Langley Research Center Hampton, VA, United States)
Diamond, John
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Applied Aerodynamics Conference, 11th, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 1 (A93-47201 19-02)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 93-3465
Accession Number
93A47246
Distribution Limits
Public
Copyright
Other

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