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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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