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An Evaluation Of Measured Pressure Signatures From Wind Tunnel Models Of Three Low Boom Concepts
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Book Synopsis An Evaluation of Measured Pressure Signatures from Wind-tunnel Models of Three Low-boom Concepts by : National Aeronautics and Space Administration
Download or read book An Evaluation of Measured Pressure Signatures from Wind-tunnel Models of Three Low-boom Concepts written by National Aeronautics and Space Administration and published by . This book was released on 2018-08-27 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Revised 1990-1991 sonic-boom design and analysis methodology was assessed by applying it to the design of three low-boom concepts. Models of these concepts were built and used to measure pressure signatures in the wind tunnel. An analysis of wind-tunnel data showed unexpected nacelle-inlet and the nacelle-wing interference-lift shocks in the pressure signatures from the two engine-under-the-wing models, but not in the measured pressure signatures from the wind-tunnel model with the engine nacelles mounted on the aft fuselage. However, additional lift-induced shocks were found in the pressure signature data from all three wind-tunnel models indicating that other flow-field disturbance effects were present.Mack, Robert J.Langley Research CenterSONIC BOOMS; FLOW DISTRIBUTION; DESIGN ANALYSIS; NACELLES; INTERFERENCE LIFT; WIND TUNNEL TESTS; SIGNATURES; WINGS...
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Book Synopsis Investigation of Flow-field Development for a Series of Sonic-boom Wind-tunnel Models by :
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Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :478 pages Book Rating :4.F/5 ( download)
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