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Research requirements for a real-time flight measurements and data analysis system for subsonic transport high-lift researchA multiphased research program to obtain detailed flow characteristics on a multielement high-lift flap system is being conducted on the Transport Systems Research Vehicle (B737-100 aircraft) at NASA Langley Research Center. Upcoming flight tests have required the development of a highly capable and flexible flight measurement and data analysis instrumentation system. This instrumentation system will be more comprehensive than any of the systems used on previous high-lift flight experiment at NASA Langley. The system will provide the researcher near-real-time information for decision making needed to modify a flight test in order to further examine unexpected flow conditions. This paper presents the research requirements and instrumentation design concept for an upcoming flight experiment for the subsonic transport high-lift research program. The flight experiment objectives, the measurement requirements, the data acquisition system, and the onboard data analysis and display capabilities are described.
Document ID
19930070394
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitehead, Julia H.
(NASA Langley Research Center Hampton, VA, United States)
Harris, Franklin K.
(NASA Langley Research Center Hampton, VA, United States)
Lytle, Carroll D.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: International Instrumentation Symposium, 39th, Albuquerque, NM, May 2-6, 1993, Proceedings (A93-54351 24-35)
Publisher: Instrument Society of America
Subject Category
Aircraft Instrumentation
Accession Number
93A54391
Distribution Limits
Public
Copyright
Other

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