About this document

Aircraft Engine Mass and Thrust Equations by Ahmad is a document available to read on EtoBox.

The document presents equations for calculating the mass (tM,E,f) and cost (CM,M,E,f) of engines for an aircraft. It includes variables for the number of engines (nE), take-off thrust per engine (TT/O,E), bypass ratio (BPR), OEPR ratio, number of compressor stages (nC), and number of spools (nS). Factors k1, k2, k3, and k4 are defined which relate to engine design parameters and are needed to calculate engine mass and cost.

Author

Ahmad

Language

EN