a thesis in the record
Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° Swept-Back Supersonic Wing of 3.44 Aspect Ratio
1949 · California Institute of Technology · level not given · Aeronautics
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@misc{academicancestry_caltechthesis_caltechthesis_620,
author = {{Academic Ancestry}},
title = {{Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° Swept-Back Supersonic Wing of 3.44 Aspect Ratio: record of a thesis}},
year = {2026},
url = {https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A620},
note = {read on 2026-10-23}
}apa
Academic Ancestry. (2026, October 23). Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° Swept-Back Supersonic Wing of 3.44 Aspect Ratio: Record of a thesis [Read on 2026-10-23]. https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A620