CFD simulations, analysis and optimal designing of custom wings of aircraft

Aerodynamic problems in general are often difficult to solve by analytical method. Experimental or numerical simulation can be used to analyze the computational models. However, due to the large expenses required in the experimental method, the numerical method is more preferred. As Computational fl

2025-06-28 16:25:47 - Adil Khan

Project Title

CFD simulations, analysis and optimal designing of custom wings of aircraft

Project Area of Specialization Internet of ThingsProject Summary

Aerodynamic problems in general are often difficult to solve by analytical method. Experimental or numerical simulation can be used to analyze the computational models. However, due to the large expenses required in the experimental method, the numerical method is more preferred. As Computational fluid dynamics (CFD) analysis of an aircraft plays a vital role in providing an ideal design of the aircraft. The evaluation of how Computational Fluid Dynamics (CFD) package can be incorporated into a conceptual design method. The repeatability of the CFD solution as well as the accuracy of the calculated aerodynamic coefficients will be implemented. The project is focused on wing design specifically and how the qualitative and quantitative characterization of the wing provides useful information to verify the wing selection and design prior to the time consuming fabrication of aircraft. Minute changes affecting flow characteristics of aircraft, comparison for CFD analysis carried out at various angles of attack for various wing geometries and determination of lift, drag, stall angle and lift-to drag ratio wing is examined in this project

Project Objectives Project Implementation Method

As part of the design for more efficient UAVs, new wing models are implemented looking for a greater aerodynamic efficiency through CFD simulation by calculating the values of aerodynamic coefficients on the airfoil and wing geometry

Implementation of CFD tool and methods to predict the dynamic-fluid behavior of the airfoil at specific flight conditions, as well as some of its main features, such as the stall angle, lift coefficient and Drag coefficient.

Implementation of high lift devices, such as flaps and slats.

To increase the load capacity of the aircraft

Turbulence correction

Benefits of the Project

Cost efficient

To reduce downtime and loss of revenue by decreasing the probability of loss of profits, repair costs, fixed and variable operating costs wasted during downtime, and a myriad of other costs that reverberate throughout the business

Improve speed and quality of the design optimization process

Eliminate the time-consuming, error-prone process of manually evaluating incremental design variations.

Improving the engineer’s insight into fluid flow problems

Technical Details of Final Deliverable Final Deliverable of the Project HW/SW integrated systemCore Industry ManufacturingOther Industries IT , Transportation , Others Core Technology Internet of Things (IoT)Other Technologies Augmented & Virtual Reality, 3D/4D Printing, OthersSustainable Development Goals Affordable and Clean Energy, Decent Work and Economic Growth, Industry, Innovation and Infrastructure, Responsible Consumption and Production, Partnerships to achieve the GoalRequired Resources
Item Name Type No. of Units Per Unit Cost (in Rs) Total (in Rs)
Total in (Rs) 79389
RC Controller Equipment185008500
Receiver / Transmitter Equipment11120011200
External HDD Equipment187908790
Programmable Microcontroller Equipment11150011500
Parameter testing Sensors Equipment83002400
Balsa Wood Miscellaneous 108508500
Servo motors Equipment5300015000
Actuators Equipment124992499
Wiring Miscellaneous 1500500
Manufacturing tools Miscellaneous 1500500
Graphi Card Equipment11000010000

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