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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