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Heat Dissipation from a Finned Cylinder at Different Fin-Plane/Air-stream Angles

NASA Technical Reports Server (NTRS) · 1932 · 6 pictures

This is a 1932 NACA technical report, issued by the National Advisory Committee for Aeronautics for engineers and aircraft researchers, studying heat dissipation from a finned aero-engine cylinder at different fin-plane angles to the airstream. Its pictures are plain engineering diagrams: circular fin-surface airflow sketches with arrows, and line graphs of temperature and heat-transfer coefficient against air speed and heat input, drawn in black ink on cream paper with a restrained grid and labelled curves that a designer could borrow for technical infographic styling.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work) · More from this library