Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line, by Jones F. Cahill et al.

Title:	Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line
Author:	Cahill, Jones F.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Adviosry Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1949

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Subject:	Airplanes -- Wings, Swept-back
Subject:	Flaps (Airplanes)
Subject:	Reynolds number
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