High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

Julio Chu

1990

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Evaluation of flow quality in two large NASA wind tunnels at transonic speeds

Bill Harvey

1980

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Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel

M. J. Goodyer

1984

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