Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44

Scherrer, Richard., Gowen, Forrest E.
naca-rm-a55f23
1955

The performance of a rectangular cross section, variable-area, variable-internal-contraction air inlet has been investigated at zero angle of attack at Mach no.s of 1.42, 1.75, 1.90, 1.99 and 2.44.

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