NASA NTRS · 19760003937
Problems in propulsion system integration
Abstract
Jet engine components are considered that influence propulsion system integration on the airframe and related aircraft drag areas. Emphasis is placed on high Mach number inlet geometries, boattailed nozzle configurations, propulsive wing installation, wing surface blowing lift, fuselage mounted nacelles, and thrust reversal.
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Henderson, W. P., Runckel, J. F.. 1975-01-01. Problems in propulsion system integration. https://ntrs.nasa.gov/citations/19760003937
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