Flight Test Results Of Riblets At Supersonic Speeds
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Flight Test Results Of Riblets At Supersonic Speeds
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Author : Fanny A. Zuniga
language : en
Publisher:
Release Date : 1992
Flight Test Results Of Riblets At Supersonic Speeds written by Fanny A. Zuniga and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.
Flight Test Results Of Riblets At Supersonic Speeds
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-03
Flight Test Results Of Riblets At Supersonic Speeds written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-03 with categories.
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...
Development Of A Low Aspect Ratio Fin For Flight Research Experiments
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Author : David M. Richwine
language : en
Publisher:
Release Date : 1994
Development Of A Low Aspect Ratio Fin For Flight Research Experiments written by David M. Richwine and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Flow visualization categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Nasa Aerodynamics Program Annual Report 1989
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Author :
language : en
Publisher:
Release Date : 1990
Nasa Aerodynamics Program Annual Report 1989 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aerodynamics categories.
Monthly Catalog Of United States Government Publications
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Author :
language : en
Publisher:
Release Date : 1995
Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Government publications categories.
Monthly Catalogue United States Public Documents
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Author :
language : en
Publisher:
Release Date : 1995
Monthly Catalogue United States Public Documents written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Government publications categories.
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings
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Author : Murray Pittel
language : en
Publisher:
Release Date : 1950
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings written by Murray Pittel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamics, Supersonic categories.
Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from Mach number 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings
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Author : Murray Pittel
language : en
Publisher:
Release Date : 1956
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings written by Murray Pittel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.
Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from a Mach number M of 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1994
Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Government reports announcements & index categories.