-Performance-calculations-and-plotting-for-subsonic-Aircraft-Using-Python.

Jet Airplane Performance Estimation: B737 Example

Project Overview

This repository hosts a Jupyter Notebook detailing the performance estimation of a medium-range jet airplane modeled after the Boeing 737. The analysis encompasses various flight performance aspects using computational methods in Python.

Analysis Aspects

The performance estimation covers the following aspects:

  1. Drag Polar: Calculation and visualization of the drag characteristics.
  2. Level Flight Performance: Analysis includes stalling speed, maximum and minimum speed determination.
  3. Steady Climb Performance: Estimation of maximum rate and angle of climb, service ceiling, and absolute ceiling.
  4. Range and Endurance: Evaluation of the aircraft’s flight range and endurance capabilities.
  5. Steady Level Co-ordinated Turn: Computation of the minimum radius and maximum rate of turn.
  6. Take-off and Landing Distances: Calculation of required distances for take-off and landing phases.

Repository Structure

How to Run the Notebook

To run this analysis, you need to have Python and Jupyter Notebook installed. Follow these steps:

  1. Clone the repository: git clone https://github.com/your-username/jet-airplane-performance-estimation.git
  2. Navigate to the repository directory: cd jet-airplane-performance-estimation
  3. Install dependencies: pip install -r requirements.txt
  4. Launch the Jupyter Notebook: jupyter notebook
  5. Open Performance_Estimation_B737.ipynb from the Jupyter interface.
  6. Run the cells in sequence to view the analysis and results.

Results

The notebook will provide:

Contact

For inquiries or contributions, please contact ragireddysuresh@gmail.com.