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Flight Test Results Of Riblets At Supersonic Speeds
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Book Synopsis Flight Test Results of Riblets at Supersonic Speeds by : Fanny A. Zuniga
Download or read book Flight Test Results of Riblets at Supersonic Speeds written by Fanny A. Zuniga and published by . This book was released on 1992 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722241469 Total Pages :38 pages Book Rating :4.2/5 (414 download)
Book Synopsis Flight Test Results of Riblets at Supersonic Speeds by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Test Results of Riblets at Supersonic Speeds written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight experiment to test and evaluate the skin friction drag characteristics of a riblet surface in turbulent flow at supersonic speeds was conducted at NASA Dryden. Riblets of groove sizes 0.0030 and 0.0013 in. were mounted on the F-104G flight test fixture. The test surfaces were surveyed with boundary layer rakes and pressure orifices to examine the boundary layer profiles and pressure distributions of the flow. Skin friction reductions caused by the riblet surface were reported based on measured differences of momentum thickness between the smooth and riblet surfaces obtained from the boundary layer data. Flight test results for the 0.0030 in. riblet show skin friction reductions of 4 to 8 % for Mach numbers ranging from 1.2 to 1.6 and Reynolds numbers ranging from 2 to 3.4 million per unit foot. The results from the 0.0013 in. riblets show skin friction reductions of 4 to 15 % for Mach 1.2 to 1.4 and Reynolds numbers ranging from 3.6 to 6 million per unit foot. Zuniga, Fanny A. and Anderson, Bianca T. and Bertelrud, Arild Armstrong Flight Research Center RTOP 505-60-21...
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