The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder

Author: Schey, Oscar W.
Additional Authors: Rollin, Vern G.
Year: 1944
Document Type: N/A
Series: NACA Technical Reports
Report Number: NACA-TR-779
Link: https://digital.library.unt.edu/ark:/67531/metadc60050/

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