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Version 2 Of The Protuberance Correlations For The Shuttle Orbiter Boundary Layer Transition Tool
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Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781794114395 Total Pages :60 pages Book Rating :4.1/5 (143 download)
Book Synopsis Version 2 of the Protuberance Correlations for the Shuttle-Orbiter Boundary Layer Transition Tool by : National Aeronautics and Space Adm Nasa
Download or read book Version 2 of the Protuberance Correlations for the Shuttle-Orbiter Boundary Layer Transition Tool written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019-01-16 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: Orbiter-specific transition data, acquired in four ground-based facilities (LaRC 20-Inch Mach 6 Air Tunnel, LaRC 31-Inch Mach 10 Air Tunnel, LaRC 20-Inch Mach 6 CF4 Tunnel, and CUBRC LENS-I Shock Tunnel) with three wind tunnel model scales (0.75, 0.90, and 1.8%) and from Orbiter historical flight data, have been analyzed to improve a pre-existing engineering tool for reentry transition prediction on the windward side of the Orbiter. Boundary layer transition (BLT) engineering correlations for transition induced by isolated protuberances are presented using a laminar Navier-Stokes (N-S) database to provide the relevant boundary-layer properties. It is demonstrated that the earlier version of the BLT correlation that had been developed using parameters derived from an engineering boundary-layer code has improved data collapse when developed with the N-S database. Of the new correlations examined, the proposed correlation 5, based on boundary-layer edge and wall properties, was found to provide the best overall correlation metrics when the entire database is employed. The second independent correlation (proposed correlation 7) selected is based on properties within the boundary layer at the protuberance height. The Aeroheating Panel selected a process to derive the recommended coefficients for Version 2 of the BLT Tool. The assumptions and limitations of the recommended protuberance BLT Tool V.2 are presented. King, Rudolph A. and Kegerise, Michael A. and Berry, Scott A. Langley Research Center WBS 599489.02.07.07.04.11.01
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Book Synopsis Hypersonic Flow Research by : F.R. Riddell
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