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Development of NACA Submerged Inlets and a Comparison with Wing Leading-Edge Inlets for a 1/4-scale Model of a Fighter AirplaneCharacteristics of NACA submerged duct entries and wing leading-edge inlets designed for a 1/4 scale flow model of a fighter-type airplane powered by a jet engine in the fuselage are presented.
Document ID
19930092457
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mossman, Emmet A
Gault, Donald E
Date Acquired
August 15, 2013
Publication Date
August 7, 1947
Report/Patent Number
NACA-RM-A7A31
Report Number: NACA-RM-A7A31
Accession Number
93R21747
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DUCTS - PRESSURE RECOVERY
AIR FLOW SYSTEMS, INTERNAL
SCOOPS - NACA
FUSELAGE DUCTS
AIR FLOW - ENGINES, JET
WIND TUNNEL TESTS - AAL (10'X7') WORK CARRIED ON A AAL
PRESSURE DISTRIBUTION - DUCTS
PRESSURE DISTRIBUTION - WING DUCTS
ENGINES - INDUCTION SYSTEMS
WING DUCTS

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