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Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section /
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Ladson, Charles L.
Published 1988
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Tests of a NACA 65₁-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel /
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Plentovich, Elizabeth B.
Published 1984
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A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
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Lawing, Pierce L.
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Adcock, Jerry B.
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Ladson, Charles L.
Published 1980
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Ladson, Charles L.
Langley Research Center
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Adcock, Jerry B.
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Hill, Acquilla S.
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Lawing, Pierce L.
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Plentovich, Elizabeth B.
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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