Subsonic high-lift flight research on the NASA Transport System Research Vehicle (TSRV)Flight tests are being conducted as part of a multiphased subsonic transport high-lift research project for correlation with ground based wind tunnel and computational results. The NASA Langley TSRV 737-100 airplane is utilized to obtain flow characteristics at full-scale Reynolds numbers to contribute to the knowledge of several dominant high-lift flow issues such as boundary layer transition, confluent boundary layer development, and 3D flow separation. Recent test results obtained for a full-chord wing section including the slat, main-wing, and flap elements are presented.
Document ID
19930027278
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yip, Long P. (NASA Langley Research Center Hampton, VA, United States)
Vijgen, Paul M. H. W. (High Technology Corp. Hampton, VA, United States)
Hardin, Jay D. (Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Van Dam, C. P. (California Univ. Davis, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: AIAA Biennial Flight Test Conference, 6th, Hilton Head Island, SC, Aug. 24-26, 1992, Technical Papers (A93-11251 01-05)
Publisher: American Institute of Aeronautics and Astronautics