In the published paper [1], there are two corrections that must take place. First, Equation (19) is missing the Euclidian norm symbols () for both the numerator and denominator in the second term on the left-hand side.
Second, on p. 12 (second paragraph, first line) the following statement was made: “The bleed extraction per engine was set to 1.32 lbm/min (0.60 kg/min) per passenger [32]”. The correct statement should read “The bleed extraction was set to 1.32 lbm/min (0.60 kg/min) per passenger [32]”. The latter statement agrees with the results presented in [1].
None of these changes affect the scientific results or the conclusions presented in [1]. The authors apologize to readers for any inconvenience these corrections may have caused. The original publication has also been updated.
Reference
- Gurrola Arrieta, M.d.J.; Botez, R.M. Improved Local Scale Generic Cycle Model for Aerothermodynamic Simulations of Gas Turbine Engines for Propulsion. Designs 2022, 6, 91. [Google Scholar] [CrossRef]
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