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NASA NTRS · 19700006492

Effects of shock-induced separation Technical summary report

Abstract

Supersonic and subsonic shock wave boundary layer separation studies on aeroelasticity of Saturn launch vehicles

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BibTeXRIS

Ericsson, L. E., Guenther, R. A., Reding, J. P.. 1969-07-01. Effects of shock-induced separation Technical summary report. https://ntrs.nasa.gov/citations/19700006492

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