NASA on F404 in 1990

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NASA on F404 in 1990

 

Introduction 

The determination of in-flight thrust isimportant to any aircraft performance analysis. Because thedirect measurement of thrust and drag inflight is not feasible, various methods have been devised to calculate thrust indirectly from themeasurement of related engine parameters. There is no globally standardthrust calculation method because ofthe variety of engines, diversity of applications, and accuracy requirements.


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