NASA NTRS · 19930091791
Internal-flow systems for aircraft
Abstract
An 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.
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Rogallo, F M. 1941-01-01. Internal-flow systems for aircraft. https://ntrs.nasa.gov/citations/19930091791
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