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    Cover image for Over-All Performance of J65-B3 Turbojet Engine for Reynolds Number Indices from 0.8 to 0.2
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    Over-All Performance of J65-B3 Turbojet Engine for Reynolds Number Indices from 0.8 to 0.2

    David B Fenn,William L Jones

    The steady-state over-all performance characteristics of the J65-B3 turbojet engine were determined in an altitude test chamber for four exhaust-nozzle areas at Reynolds number indices of 0.8, 0.4, and 0.2…

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