In this paper, the extrapolation formulas of rocket engine performance parameters are established utilizing one isentropic reference line and two partial derivatives for fixed enthalpy.
本文利用一条等熵参考线和两个等焓偏导数建立了火箭发动机性能参数的外推公式。
In this paper, a method of curve fitting with asymptotic line is proposed for reducing the error of extrapolation value.
本文提出一种降低拟合曲线外推偏差的方法——渐近线辅助拟合法。
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