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Studies in Panel Flutter at Higher Mach Numbers: I. Flat and Slightly Curved Panels at Mach Number 2.81. II. Cylindrical Shells with Boundary Layer
1963 · California Institute of Technology · doctoral · Aeronautics; Mathematics
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@misc{academicancestry_caltechthesis_caltechthesis_5008,
author = {{Academic Ancestry}},
title = {{Studies in Panel Flutter at Higher Mach Numbers: I. Flat and Slightly Curved Panels at Mach Number 2.81. II. Cylindrical Shells with Boundary Layer: record of a thesis}},
year = {2026},
url = {https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A5008},
note = {read on 2026-10-22}
}apa
Academic Ancestry. (2026, October 22). Studies in Panel Flutter at Higher Mach Numbers: I. Flat and Slightly Curved Panels at Mach Number 2.81. II. Cylindrical Shells with Boundary Layer: Record of a thesis [Read on 2026-10-22]. https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A5008