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Study on the Effect of Two Uncertainty Parameters on Scramjet Engine Using Monte Carlo Simulation
International Journal of Mathematical Models and Methods in Applied Sciences
Today, aerospace engines are developing rapidly, these engines are divided into two groups of gas turbines and without gas turbines. In this thesis, the thermodynamic performance of the scramjet engine is examined. This study is carried out with consideration of uncertainty parameters. Two parameters of the combustion chamber efficiency and heating value of fuel are considered as uncertainty parameters. Using Monte Carlo numerical simulation method, the functional curves of the scramjet enginedoi:10.46300/9101.2022.16.16 fatcat:pcc5kqtsxrbzvf7z4yz5hhcwzy