I claim: 1. A system for operating a jet turbine engine, said system comprising: a compressor for receiving an intake airflow to the jet engine; a hypersonic compression ram radially inward of the compressor for receiving another portion of the intake airflow; a combustion chamber fluid communi...
Although most of the testing enthusiasts claim that the right coverage threshold is contextual, most of them also mention the number 80% as a thumb of a rule (Fowler: “in the upper 80s or 90s”) that presumably should satisfy most of the applications. Implementation tips: You may want to...