Engineering Transactions, 39, 2, pp. 207-219, 1991

An Estimate of the Influence of the Compressor Stability Margin on the Thrust of a Turbojet Engine

M. Orkisz
Air Force Academy, Dęblin
Poland

The relations derived in the paper make it possible to analyze. the influence of the compressor stability margin upon the thrust of a turbo jet engine. The engines operating within the economy range (minimum fuel consumption) and optimum range (maximum thrust) are considered.

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