Heat Dissipation from a Finned Cylinder at Different Fin-Plane/Air-stream Angles (1932)
NASA Technical Reports Server (NTRS) · leaf 20
K.A.CA. Technical ITote iJo.429 Fig. 9 … Fig. 9 The effect of air speed on the heat transfer coefficient U^^ at a hoat input of 107 B.t.u. for several fin-plane/air-stream angles.
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