F16 发动机推力计算 C++

以下是一个简单的 F16 发动机推力计算 C++ 代码示例：

#include <iostream>
#include <cmath>

using namespace std;

int main()
{
    double throttle, altitude, temperature, pressure;
    double thrust, thrust_max, thrust_mil;

    cout << "Enter throttle setting (0-100%): ";
    cin >> throttle;

    cout << "Enter altitude (feet): ";
    cin >> altitude;

    cout << "Enter temperature (F): ";
    cin >> temperature;

    cout << "Enter pressure (inHg): ";
    cin >> pressure;

    thrust_max = 29000.0; // maximum thrust at sea level
    thrust_mil = 19000.0; // military thrust at sea level

    // Calculate thrust based on altitude and temperature
    thrust = thrust_max * (1 - 0.00062 * altitude / 1000) * pow((temperature + 459.67) / 518.67, -0.7);

    // Adjust thrust for pressure and throttle setting
    thrust = thrust * pressure / 29.92 * throttle / 100;

    // Output calculated thrust
    cout << "Thrust: " << thrust << " pounds" << endl;

    // Output whether the thrust is greater than military thrust
    if (thrust > thrust_mil)
    {
        cout << "Thrust exceeds military thrust" << endl;
    }
    else
    {
        cout << "Thrust is less than military thrust" << endl;
    }

    return 0;
}

这段代码可以计算 F16 发动机在给定的油门、高度、温度和气压下的推力，并显示结果。请注意，这只是一个简单的示例，实际的 F16 发动机推力计算可能需要更复杂的模型和数据。