Calculation of Drag Coefficients for Hypersonic Spherical Projectiles Initiating Oblique Detonation Wave or Shock-Induced Combustion
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 14516-14520
2012-01-01
5 pages
Includes bibliographical references and index
Conference paper
English
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Chapman-Jouguet oblique detonation structure around hypersonic projectiles
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