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  1. 1
    High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
    by Mineck, Raymond E.
    Published 1987
    Government Document Book
  2. 2
    Assessment of dual-point drag reduction for an executive-jet modified airfoil section /
    by Allison, Dennis O.
    Published 1996
    Government Document Book
  3. 3
    Reynolds number effects on the performance of lateral control devices /
    by Mineck, Raymond E.
    Published 2000
    Government Document Book
  4. 4
    Reynolds number effects on the performance of lateral control devices /
    by Mineck, Raymond E.
    Published 2000
    Get full text
    Government Document eBook
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