The SAE Aero Design competition has challenged teams to design, build, and test radio-controlled aircraft that met strict performance criteria while adhering to specific constraints. I was a part of DJS Skylark as the Aerodynamics Lead for the 2019 and 2020 SAE Aero Design seasons, where we competed in the SAE Aero Design competition held in the U.S.
In Regular Class, the objective was to develop a fixed-wing aircraft capable of carrying the maximum payload possible while staying within predefined size, weight, and power limits. Teams had to balance aerodynamic efficiency, structural integrity, and payload optimization to achieve the highest score.
In Micro Class, the focus was on creating a compact, lightweight, and rapidly deployable aircraft that could fit within a small storage volume when disassembled and be quickly reassembled before flight. The challenge required innovative design strategies to maintain portability, structural strength, and aerodynamic performance while optimizing payload capacity.
Fig 1: Team Photo
As a team, DJS Skylark adopted an iterative design methodology focused on achieving peak performance through continuous analysis, testing, and refinement. As the aero head, I played a key role in guiding the aerodynamic development of the aircraft. Here's a breakdown of our process:
Defining Our Goals: We began by setting clear goals, including minimizing empty weight and maximizing payload capacity, with a target to carry over 50 lbs.
Analyzing the Competition: We examined past competition results and scoring metrics to pinpoint key areas for improvement and strategic decision-making, such as optimizing luggage weight per passenger to maximize our score.
Initial Prototyping: We developed an initial prototype using a CH10 airfoil, specifically targeting our empty weight goal.
Airfoil Selection and Flow Analysis: Recognizing the critical role of airfoil performance, I spearheaded the selection of the S1223RTL airfoil. This decision was based on extensive CFD (Computational Fluid Dynamics) analysis, where we prioritized its high lift coefficient and reduced flow separation in 3D flow conditions. My direction here was crucial in shaping the aircraft's aerodynamic characteristics.
Iterative Refinement and Analysis: We continuously refined our subsequent prototypes, incorporating the S1223RTL airfoil and structural enhancements. Ongoing testing and analysis, guided by my expertise, allowed us to optimize performance while balancing weight and structural integrity. We focused on addressing flow separation and minimizing induced drag.
Trade Studies and Optimization: I oversaw the trade studies to evaluate various factors, such as airfoil selection, wing planform, and luggage configuration, striving for the best possible flight score.
Ensuring Structural Integrity: We conducted structural analysis throughout the design process to guarantee adequate strength while maintaining a safety margin below 0.2.
Prioritizing Drag Reduction: Acknowledging power limitations, we placed significant emphasis on drag reduction to increase velocity and, consequently, lift. I championed the adoption of aerodynamic covers and Hoerner tips to minimize drag.
Our methodology hinged on a continuous cycle of design, analysis, manufacturing, testing, and optimization. My leadership as the aero head helped drive the aerodynamic design to achieve the desired performance within the competition constraints.
Fig 2: Airflow Simulation on Airfoils
Fig 3: Tail Airfoil Analysis
As aero head on a team of 30 students, the SAE Aero Design project was a significant project management experience for me. It demanded seamless integration of aerodynamics with structural, avionics, and manufacturing aspects, and the attached document is the design report. Our key project management strategies included:
Cross-Functional Teams: Departments (avionics, structural, aerodynamics, marketing) collaborated closely, ensuring design decisions didn't negatively impact other areas.
Clear Roles and Responsibilities: Each team member had clearly defined roles and responsibilities, fostering accountability and ownership.
Iterative Design Process: We followed a phased approach with monthly cycles of design, testing, and optimization. This iterative process, which began in July 2018, allowed us to identify and address potential issues early in the development process.
Cost Management: We carefully managed our budget by sourcing materials from wholesalers, seeking sponsorships, and organizing fundraising events.
Risk Management: We identified potential risks, such as manufacturing delays and component failures, and developed contingency plans to mitigate these risks.
Schedule Management: We used a detailed schedule to track progress and ensure that we met our deadlines. As aero head, I coordinated with other team leads to ensure that the aerodynamic design was completed on time and integrated with other subsystems.
Communication and Documentation: Regular team meetings, progress reports, and design reviews facilitated effective communication and knowledge sharing. We maintained detailed documentation of our design decisions, analysis results, and manufacturing processes.
Fundraising: We organized an annual aeromodelling workshop in September to raise funds. I actively participated in the fundraising efforts, which significantly contributed to our financial resources.
As the aero head and a key member of the design report team, I played a central role in designing, documenting, and presenting our SAE Aero Design project. I ensured that the aerodynamic integrity of our aircraft was communicated effectively through rigorous analysis and clear writing. I actively contributed to the design report, detailing our aerodynamic design choices, analysis methodologies including those using CFD simulations and VG diagrams, and performance predictions. I compiled and analyzed data, creating figures and tables to visualize key findings and support our design decisions. Additionally, I assisted in developing our technical presentation, ensuring that we clearly and concisely communicated our design process and performance capabilities to the judges.
Fig 4: Load Factor DIagram from Design Documentation
Fig 5: Weight Distribution of the Airplane
DJS Skylark achieved notable success, and our global results were as follows:
2019:
2nd place for Design Report (Micro Class)
4th place (Regular Class Design)
2020:
1st place in Micro Class Dynamic Event
2nd in Micro Class Mission Performance
3rd place in Micro Class Technical Presentation
3rd place overall in Micro Class
The Regular Class provided a significant challenge, offering valuable lessons for future iterations.
Personal Learning: This project provided invaluable hands-on experience, translating theoretical knowledge into practical application. Beyond the technical skills, it reinforced the importance of teamwork, communication, meticulous planning, and the intersection of analysis, design, and manufacturing. The dynamic environment demanded adaptability and innovative problem-solving, skills I have carried forward in my engineering endeavors. This project was an incredible experience in the value of proper planning, as the iterative design cycles taught me more about the process of aircraft design.
Fig 6: Awards won in 2020
Fig 7: Award won in 2019