The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets

The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets

abstract: The objective of this study is to understand how to integrate conical spike external compression inlets with high bypass turbofan engines for application on future supersonic airliners. Many performance problems arise when inlets are matched with engines as inlets come with a plethora of l...

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Bibliographic Details
Other Authors: Cleary, Spencer (Author)
Format: Dissertation
Language:English
Published: 2018
Subjects:
Aerospace engineering
External Compression Inlets
High Bypass Turbofan Engines
Supersonic Aircraft Performance
Supersonic Airliners
Supersonic Propulsion Performance
Online Access:http://hdl.handle.net/2286/R.I.49114

Internet

http://hdl.handle.net/2286/R.I.49114

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