Characteristics 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.
Development of NACA Submerged Inlets and a Comparison with Wing Leading-Edge Inlets for a 1/4-scale Model of a Fighter Airplane
07.08.1947
Sonstige
Keine Angabe
Englisch
NTIS | 1988
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