Measurement of attachment-line location in a wind-tunnel and in supersonic flightFor the supersonic laminar flow control research program, tests are being conducted to measure the attachment-line flow characteristics and its location on a highly swept aircraft wing. Subsonic wind tunnel experiments were conducted on 2D models to develop sensors and techniques for the flight application. Representative attachment-line data are discussed and results from the wind tunnel investigation are presented.
Document ID
19930027288
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Agarwal, Naval K. (NASA Langley Research Center Hampton, VA, United States)
Miley, Stan J. (NASA Langley Research Center Hampton, VA, United States)
Fisher, Michael C. (NASA Langley Research Center Hampton, VA, United States)
Anderson, Bianca T. (NASA Langley Research Center Hampton, VA, United States)
Geenen, Robert J. (NASA Flight Research Center Edwards, CA, 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