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Internal-flow systems for aircraftAn investigation has been made to determine efficient arrangements for an internal-flow system of an aircraft when such a system operates by itself or in combination with other flow systems. The investigation included a theoretical treatment of the problem and tests in the NACA 5-foot vertical wind tunnel of inlet and outlet openings in a flat plate and in a wing.
Document ID
19930091791
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rogallo, F M
Date Acquired
September 6, 2013
Publication Date
January 1, 1941
Report/Patent Number
NACA-TR-713
Report Number: NACA-TR-713
Accession Number
93R21081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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