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收敛段长度计算有误，已改正并改为PyQt5：
Pythonfrom PyQt5.QtWidgets import QApplication, QMainWindow, QLabel, QLineEdit, QPushButton, QVBoxLayout, QHBoxLayout, \
QWidget, QFileDialog, QMessageBox
from PyQt5.QtCore import Qt
from math import sqrt, tan, radians
class RocketChamberDesign(QMainWindow):
def __init__(self):
super().__init__()
self.setWindowTitle("推力室内弹道")
self.setGeometry(100, 100, 600, 400)
self.setStyleSheet("""
QMainWindow {
background-color: #f0f0f0;
}
QLabel {
font-size: 14px;
color: #333333;
}
QLineEdit {
font-size: 14px;
border: 1px solid #cccccc;
padding: 5px;
background-color: white;
border-radius: 5px;
}
QPushButton {
font-size: 16px;
padding: 10px 20px;
border: none;
background-color: #007acc;
color: white;
border-radius: 5px;
}
QPushButton:hover {
background-color: #005fa3;
}
""")
self.initUI()
def initUI(self):
central_widget = QWidget(self)
main_layout = QVBoxLayout()
central_widget.setLayout(main_layout)
self.setCentralWidget(central_widget)
# Labels and LineEdits
self.create_input("质量流量（Kg/s）：", main_layout)
self.create_input("气体比热比（γ）：", main_layout)
self.create_input("燃室压力（MPa）：", main_layout)
self.create_input("燃室温度（K）：", main_layout)
self.create_input("气体常数（J/(Kg·K)）：", main_layout)
self.create_input("出口压力（MPa）：", main_layout)
self.create_input("特征长度（m）：", main_layout)
self.create_input("径收敛比（Dc/Dt）：", main_layout)
self.create_input("敛段半角（°）：", main_layout)
# Button layout
button_layout = QHBoxLayout()
calculate_button = QPushButton("计算", self)
calculate_button.clicked.connect(self.calculate)
button_layout.addWidget(calculate_button, alignment=Qt.AlignHCenter)
save_button = QPushButton("保存", self)
save_button.clicked.connect(self.save)
button_layout.addWidget(save_button, alignment=Qt.AlignHCenter)
# Add the button layout to the main layout
main_layout.addLayout(button_layout)
# Output labels and line edits
output_layout = QVBoxLayout()
self.create_output("燃烧室直径Dc（mm）：", output_layout)
self.create_output("圆筒段长度Lcyl（mm）：", output_layout)
self.create_output("喷喉直径Dt（mm）：", output_layout)
self.create_output("收敛段长度（mm）：", output_layout)
self.create_output("出口直径De（mm）：", output_layout)
self.create_output("膨胀比Ae/At：", output_layout)
# Add the output layout to the main layout
main_layout.addLayout(output_layout)
def create_input(self, label_text, layout):
input_layout = QHBoxLayout()
label = QLabel(label_text, self)
label.setAlignment(Qt.AlignRight | Qt.AlignVCenter)
input_layout.addWidget(label)
line_edit = QLineEdit(self)
line_edit.setAlignment(Qt.AlignLeft)
input_layout.addWidget(line_edit)
layout.addLayout(input_layout)
attr_name = self._format_attribute_name(label_text)
setattr(self, attr_name, line_edit)
print(f"Created attribute: {attr_name}")
def create_output(self, label_text, layout):
output_layout = QHBoxLayout()
label = QLabel(label_text, self)
label.setAlignment(Qt.AlignRight | Qt.AlignVCenter)
output_layout.addWidget(label)
line_edit = QLineEdit(self)
line_edit.setReadOnly(True)
output_layout.addWidget(line_edit)
layout.addLayout(output_layout)
attr_name = self._format_attribute_name(label_text) + '_output'
setattr(self, attr_name, line_edit)
print(f"Created attribute: {attr_name}")
@staticmethod
def _format_attribute_name(text):
# Replace non-alphanumeric characters with underscores and remove leading numbers
return ''.join([char if char.isalnum() else '_' for char in text]).lstrip('_')
def calculate(self):
try:
gamma = float(getattr(self, self._format_attribute_name("比热比（γ）：")).text())
mass_flow = float(getattr(self, self._format_attribute_name("质量流量（Kg/s）：")).text())
pressure = float(getattr(self, self._format_attribute_name("压力（MPa）：")).text())
temperature = float(getattr(self, self._format_attribute_name("温度（K）：")).text())
gas_constant = float(getattr(self, self._format_attribute_name("气体常数（J/(Kg·K)）：")).text())
pressure_export = float(getattr(self, self._format_attribute_name("出口压力（MPa）：")).text())
characteristic_length = float(getattr(self, self._format_attribute_name("特征长度（m）：")).text())
diameter_convergence_ratio_length = float(
getattr(self, self._format_attribute_name("直径收敛比（Dc/Dt）：")).text())
convergence_half_angle = float(getattr(self, self._format_attribute_name("敛段半角（°）：")).text())
G = sqrt(gamma) * (2 / (gamma + 1)) ** ((gamma + 1) / (2 * (gamma - 1)))
throat_area = mass_flow / (G * (pressure / sqrt(gas_constant * temperature)))
compute_throat_diameter = sqrt(throat_area / 3.14159) * 2
expansion_area_ratio = ((2 / (gamma + 1)) ** (1 / (gamma - 1)) * (
(pressure / pressure_export) ** (1 / gamma))) / sqrt(
((gamma + 1) / (gamma - 1)) * (1 - ((pressure_export / pressure) ** ((gamma - 1) / gamma))))
compute_export_diameter = sqrt(throat_area * expansion_area_ratio / 3.14159) * 2
chamber_volume = throat_area * characteristic_length
compute_chamber_radius = round(compute_throat_diameter * diameter_convergence_ratio_length + 0.4, 0) / 2
compute_convergence_length = (compute_chamber_radius * 2 - compute_throat_diameter) / (
2 * tan(radians(convergence_half_angle)))
chamber_volume -= float(compute_convergence_length) * 3.14159 * float(compute_chamber_radius ** 2 +
(compute_throat_diameter / 2) ** 2 +
compute_throat_diameter / 2 * compute_chamber_radius) / 3000
compute_cylinder_length = chamber_volume * 1000 / (compute_chamber_radius ** 2 * 3.14159)
getattr(self, self._format_attribute_name("燃烧室直径Dc（mm）：") + '_output').setText(
f'{compute_chamber_radius * 2}')
getattr(self, self._format_attribute_name("圆筒段长度Lcyl（mm）：") + '_output').setText(
f'{round(compute_cylinder_length + 0.4, 0)}')
getattr(self, self._format_attribute_name("喷喉直径Dt（mm）：") + '_output').setText(
f'{round(compute_throat_diameter, 3)}')
getattr(self, self._format_attribute_name("收敛段长度（mm）：") + '_output').setText(
f'{round(compute_convergence_length + 0.4, 0)}')
getattr(self, self._format_attribute_name("出口直径De（mm）：") + '_output').setText(
f'{round(compute_export_diameter, 3)}')
getattr(self, self._format_attribute_name("膨胀比Ae/At：") + '_output').setText(
f'{round(expansion_area_ratio, 3)}')
except Exception as e:
QMessageBox.critical(self, "错误", f"计算过程中发生错误：\n{str(e)}")
print(e)
def save(self):
filename, _ = QFileDialog.getSaveFileName(self, "保存文件", "", "Text Files (*.txt)")
if filename:
with open(filename, 'w', encoding="utf-8") as file:
file.write("推力室设计参数：\n")
file.write(f"燃烧室直径Dc（mm）：{getattr(self, '燃烧室直径Dc_mm___output').text()}\n")
file.write(f"圆筒段长度Lcyl（mm）：{getattr(self, '圆筒段长度Lcyl_mm___output').text()}\n")
file.write(f"喷喉直径Dt（mm）：{getattr(self, '喷喉直径Dt_mm___output').text()}\n")
file.write(f"收敛段长度（mm）：{getattr(self, '收敛段长度_mm___output').text()}\n")
file.write(f"出口直径De（mm）：{getattr(self, '出口直径De_mm___output').text()}\n")
file.write(f"膨胀比Ae/At：{getattr(self, '膨胀比Ae_At__output').text()}")
if __name__ == '__main__':
import sys
app = QApplication(sys.argv)
main_window = RocketChamberDesign()
main_window.show()
app.exec_()
app.quit()
