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  1. 1
    Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 /
    “...National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research...”
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    Government Document Book
  2. 2
    Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 /
    “...National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research...”
    Get full text
    Government Document Book
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