A gas turbine engine including a fan, compressor, combustor and a turbine arranged in series and surrounded by a nacelle. An engine core cowl is disposed within the nacelle. Each of these elements shares a central longitudinal axis. The nacelle length may be non-uniform around the circumference of the nacelle.
Compact Nacelle With Contoured Fan Nozzle
2015-11-19
Patent
Electronic Resource
English
Condensation in a contoured-nozzle shock tunnel
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