Based on various gas turbine configurations (i.e turboprop, turbojet, turbofan, turboshaft), indicate which engine type would be most applicable for the following aerospace applications, and why it is the most appropriate i) Military application of the Joint Strike Fighter (JSF) ii) A short range commercial flight, i.e. Cardiff to Dublin iii) A hypersonic unmanned aerospace vehicle (UAV) iv) A long range commercial flight, i.e. London-New York

Based on various gas turbine configurations (i.e turboprop, turbojet, turbofan, turboshaft), indicate which engine type would be most applicable for the following aerospace applications, and why it is the most appropriate i) Military application of the Joint Strike Fighter (JSF) ii) A short range commercial flight, i.e. Cardiff to Dublin iii) A hypersonic unmanned aerospace vehicle (UAV) iv) A long range commercial flight, i.e. London-New York

Automotive Technology: A Systems Approach (MindTap Course List)

6th Edition

ISBN:9781133612315

Author:Jack Erjavec, Rob Thompson

Publisher:Jack Erjavec, Rob Thompson

Chapter9: Automotive Engine Designs And Diagnosis

Section: Chapter Questions

Problem 3RQ: As an engines compression ratio increases, what should happen to the octane rating of the gasoline?

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