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June 1, 1968AIAA Journal

Factors affecting flow separation in contoured supersonic nozzles.

ROY A. LAWRENCE EDMUND E. WEYNAND

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Abstract

Separated flow in two dimensional and axisymmetric nozzles with various wall contours, determining flow structure and shock-boundary layer interaction

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Cite This Study

LAWRENCE et al. (1968) studied this question.

synapsesocial.com/papers/6ab2446448e5df3736a172ce https://doi.org/10.2514/3.4693

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