Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
Author(s) -
Jeremy Pinier,
Charles Niskey,
Jeremy Hanke,
William Tomek
Publication year - 2011
Publication title -
50th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2011-998
Subject(s) - aerodynamics , aerospace engineering , wind tunnel , transonic , mach number , supersonic speed , aeronautics , supersonic wind tunnel , angle of attack , flight envelope , engineering , marine engineering
Notice to Reviewers The Ares I launch vehicle, including its predicted performa nce and certain other features and characteristics, have been defined by the U.S. Government to be Sensitive But Un classified (SBU). Information deemed to be SBU requires special protection and may not be disclosed to an in ternational audience, such as the audience sure to be present at the 2011 Aerospace Sciences Meeting. To comply wi th SBU restrictions, details have been removed from some plots and figures in this abstract. It is the opinion of th e authors that despite these alterations, there is no loss of meaningful technical content. Analytical methodologie s and capabilities are discussed; significant and interesti ng technical results are obvious and still present; and meanin gful conclusions are still present.
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