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Investigation of Slipstream Effects on a Wing-Inlet Oil-Cooler Ducting System of a Twin-Engine Airplane in the Ames 40- by 80-Foot Wind Tunnel
Author:
Chapman, Dean R.
Year:
1945
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-A-1, NACA-MR-A5C10
Link:
https://digital.library.unt.edu/ark:/67531/metadc62473/
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