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### Overview: I am seeking an experienced aeronautical engineer or aircraft designer to develop a clean-sheet, 3D-printable fixed-wing UAV airframe. This aircraft is built around a simplicity-first, stability-driven design philosophy. It uses a twin-motor tractor configuration and eliminates all movable flight control surfaces (no ailerons, rudder, elevator, or servos). Control is achieved entirely through thrust modulation: * Total thrust for climb and descent * Differential thrust and accelerated lift effects for turning The aircraft is intentionally low in maneuverability and must be inherently stable, with stability driven by strong dihedral and a low center of gravity. It should naturally return to wings-level flight without active correction. ### Specifications: Configuration: * Fixed-wing UAV * Twin tractor motors mounted on wing leading edge * Counter-rotating propellers (CW left, CCW right) * Motors angled slightly upward and outward to assist turning and mitigate asymmetrical thrust-induced yaw * No movable flight control surfaces Flight Behavior: * Climb / descend via total thrust * Turning via differential thrust and induced lift asymmetry * Predictable, self-correcting flight Size & Performance Targets: * Wingspan: ~1.7–1.9 m * Payload: ~1 kg * Estimated MTOW: ~2.5–3 kg Manufacturing & Assembly: * Designed for Bambu Lab printer (256 × 256 mm bed) * Minimize number of sections while staying within print volume constraints * Seamless assembly using alignment pins and interlocking features * Minimal or no glue (press-fit preferred) * Wing must be removable using a single tool and support repeatable assembly/disassembly Structural & Internal Layout: * Payload bay located near CG * Internal wiring channels for ESC cables and lighting * Integrated motor mounts in wing leading edge * Structural design optimized for weight and strength * Carbon fiber spar reinforcement expected (designer to specify) * Material selection per section (PLA / PETG / ABS as appropriate) Engineering Scope: * Aerodynamic design and validation (XFLR5 or equivalent) * Define airfoil, wing planform, and dihedral * Generate lift/drag polars, stall estimate, CG range, and static margin * Structural optimization for load paths and print efficiency * Print optimization (orientation, supports, layer direction) ### Deliverables: * Native CAD files (Fusion 360 preferred; SolidWorks/STEP acceptable) * Print-ready STL files (organized by section) * CG location and recommended range * Recommended dihedral angle * Documentation: * Aerodynamic analysis summary (polars, stall, stability) * Structural and reinforcement recommendations * Material selection per section * Print settings and orientation per part * Assembly instructions ### Ideal Candidate & How to Apply: This project requires a strong aeronautical engineering background — not just CAD proficiency. You should have: * UAV / aircraft design experience * Deep understanding of static stability (CG, neutral point, static margin) * Experience with low Reynolds number aerodynamics * Proficiency in: * XFLR5 or similar tools * CFD (Ansys Fluent, CFX, or equivalent) * FDM design-for-manufacturing * Structural / topology optimization To apply: * Provide relevant project examples (UAV, RC aircraft, or aerodynamic designs) * Include a brief list of key technical challenges you anticipate in this design
Project ID: 40415304
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30 freelancers are bidding on average $152 USD for this job

Welcome I MADE MANY SMART DEVICES THAT MANUFACTURED AND USED IN REAL YOU WILL GET IT DONE PERFECTLY IN LESS TIME CHECK MY LATEST REVIEWS > (http://www.freelancer.com/u/ENG1mga) I have previously worked on, Lifting Set of Drones Mechanism, Robotic Arm, Delivery Robot, Automatic Wiring Machine, Solenoid Engines, Car Rooftent, Boat Lift Mechanism, Shoe Treadmill Mechanism Mechanical Ventilator and many other projects. I use Solidworks, Fusion 360, and ANSYS, COMSOL I have a workshop specializing in all 3D printing and CNC machining work, so I strive to provide the highest quality and precision. What you will receive with me: - 2D drawings - 3D files - Complete Tech. Formats - Finite Element Analysis (FEA) (if needed).
$250 USD in 2 days
6.6
6.6

Hi there, I would be happy to assist with the design of your 3D-printable fixed-wing UAV airframe. With expertise in aerodynamics, FEA/CFD, and design for additive manufacturing, I can deliver a stability-focused and print-optimized solution aligned with your concept. Approach: Aerodynamic design using XFLR5 to define airfoil, wing planform, dihedral, and stability margins Validation of lift/drag polars, stall behavior, and CG range for inherent self-stability � Freelancer Structural design with lightweight optimization and carbon fiber spar integration Print-oriented CAD segmentation for 256 × 256 mm bed with interlocking, press-fit assembly Optimization of print orientation, material selection, and internal structure for strength vs weight Integration of propulsion layout and internal routing for wiring and payload Deliverables: Native CAD files (Fusion 360 / STEP) Section-wise STL files ready for printing Aerodynamic report (polars, CG, stability, stall) Structural and material recommendations Print settings, orientation, and assembly guide Timeline: To be determined after discussing project scope. Budget: Open to negotiation based on complexity. Looking forward to collaborating on this innovative UAV project. Let’s connect to discuss further. Best regards, Arati M.
$140 USD in 7 days
6.3
6.3

Hi there! I can deliver a 3D-printable fixed-wing UAV airframe with optimized aerodynamics, lightweight structure, and split components for easy assembly—ready for reliable printing and flight testing. Questions ? What wingspan and payload capacity are you targeting? ? Which material and printer size constraints should I design for? ? Do you need internal mounts for electronics (motor, battery, FC)? Don't pay a single penny until you are happy with the job I look forward to your response and thank you for your consideration. Warm regards, The Blend Nation.
$33 USD in 1 day
6.0
6.0

Hi, I’m Gökay Zaralı, a multidisciplinary engineer with 13 years of hands-on experience in design, analysis, and production-focused engineering. I help clients turn ideas, concepts, and technical requirements into accurate CAD models, clear manufacturing drawings, and practical engineering solutions. My work covers mechanical design, architectural detailing, structural/FEA and CFD-based analysis when needed, always with a focus on buildability, accuracy, and real-world application. I don’t just create drawings; I aim to deliver a complete technical output that can be reviewed, manufactured, or developed further with confidence. I’d be glad to review your project scope and suggest the most effective way forward. Best regards, Gökay Zaralı
$500 USD in 7 days
5.8
5.8

I will design a high performance, 3D-printable fixed wing UAV airframe that balances aerodynamic efficiency with structural rigidity for stable flight. I am ready to deliver optimized STL files featuring internal spar channels and thin-wall geometry, ensuring a lightweight yet durable build for your specific mission requirements.
$120 USD in 2 days
5.5
5.5

Hello I’m interested in helping design your UAV airframe and can deliver the required CAD and analysis deliverables. I am an experienced CAD/CAM designer specializing in CATIA, SolidWorks, and AutoCAD, with over 10 years of professional freelance and teaching experience. I excel at transforming 2D plans into precise, detailed 3D models, creating accurate assemblies, parts, and visualizations ready for manufacturing or prototyping. With my expertise in Part Design, Generative Shape Design (GSD), Drafting, and Assembly Design, I deliver high-quality, production-ready models in STL, STEP, OBJ, or FBX formats. I am detail-oriented, efficient, and committed to exceeding client expectations. Best regards, Mounir
$52 USD in 3 days
5.3
5.3

Greetings from Vutuk Design and Media! Our firm brings 15 years of professional engineering and technical visualization expertise to your 3D-Printable Fixed-Wing UAV project. We offer a comprehensive design-to-flight workflow, ensuring that your airframe is aerodynamically sound and structurally robust. We utilize advanced FEA to validate the wing loading and CFD to optimize the airfoil selection for maximum endurance. To help us refine the project roadmap, please clarify: Do you require 3D animations of the assembly process or a flight simulation to showcase the UAV’s capabilities? Should we design internal mounting points for specific flight controllers (e.g., Pixhawk or Ardupilot)? Is the airframe intended for a modular "break-away" design to facilitate easy transport and repair? What is the target cruising speed and stall speed you are aiming for with this airframe? At Vutuk Design and Media, we bridge the gap between complex aerospace engineering and practical digital manufacturing. I invite you to visit our profile and review our portfolio, which showcases our track record in machine design, 3D production visuals, and functional prototyping. We are eager to collaborate with you to deliver a professional-grade UAV airframe that stands out for its performance and printability. Let’s get to work!
$140 USD in 7 days
4.5
4.5

With my extensive experience in 3D modeling and 3D printing, I am confident that I can deliver the design and print optimization you require for your fixed-wing UAV airframe. Not only am I proficient with design software such as SolidWorks, Fusion 360, and more, but I have also worked extensively with various materials utilized in FDM printing such as PLA, PETG, ABS. This enables me to optimize your design not just aerodynamically but also structurally to ensure weight efficiency while maintaining the necessary strength using carbon fiber spar reinforcement where needed. In addition to my technical skills mentioned above, I offer great depth and understanding of static stability and low Reynolds number aerodynamics - crucial aspects for this project. I am conversant with tools like XFLR5 and CFD packages that will be essential in the aerodynamic design validation process. With regards to FDM manufacturing, my keen eye for detail ensures minimal prints sections to fit the print bed while enhancing features like internal wiring channels for ESC cables and lighting which will aid in your assembly/disassembly requirement. Past clients have lauded me for my ability to deliver dimensionally accurate models that are visually impressive and purpose-optimized - key qualities you seek for this project. Let's leverage my aeronautical engineering background in tandem with these skills to bring your unique UAV airframe design to reality.
$37 USD in 1 day
4.4
4.4

Hi, how are you doing? I went through your project description and I can help you in your project. your project requirements perfectly match my expertise. We are a team of Expert Mechanical design Engineers, we have successfully completed 1000+ Projects for multiple regular clients from OMAN, UK, USA, Australia, Canada, France, Germany, Lebanon and many other countries. We are providing our services in following areas: Product Design | 3D CAD Modelling Finite Element Analysis | Computational Fluid Dynamics Thermal analysis | Structural analysis HVAC and Heat load calculation We are proficient in using following software’s: AUTOCAD SOLIDWORKS ABAQUS ANSYS APDL | ANSYS Fluent MATLAB | SIMULINK COMSOL Multiphysics FUSION360 | CATIA We have good command over REPORT WRITING, we can show you many samples of our previous reports. We can discuss further details in the message box.
$140 USD in 7 days
4.4
4.4

Hello, Having read through your detailed requirements for a 3D-printable fixed-wing UAV airframe, I'm confident that my extensive experience in 3D modeling and optimization, with proficiency in SolidWorks, makes me an ideal fit for this project. I am a seasoned 3D modeler with over 5 years of hands-on experience, specializing in transforming imaginative concepts into perfectly optimized and print-ready 3D models. I have comprehensive knowledge of slicing software and my models are assured to maintain high print quality and structural integrity. In terms of the unique technical challenges that this project presents, I look forward to applying my skills in FDM design-for-manufacturing and structural/topology optimization to ensure your airframe is designed with optimal weight and strength. My attention to detail will be crucial when considering factors such as load paths, print efficiency, material selection and assembly instructions. Moreover, as a passionate and dedicated professional, I take pride in turning clients' ideas into reality by closely collaborating with them throughout the process. I'm committed to not only meeting but exceeding your expectations by delivering native CAD files (Fusion 360 preferred) and print-ready STL files along with meticulous documentation. With me on the team, you can rest assured that your simplicity-first, stability-driven UAV airframe design will soar above the competition. Thanks!
$30 USD in 4 days
4.4
4.4

Hi I’m a mechanical engineer and have done similar UAV design, simulation, and 3D printable product development projects. I can help you develop a clean-sheet, stability-driven fixed-wing UAV with a strong focus on aerodynamic stability, structural efficiency, and print-ready modular design. I have experience with SolidWorks, ANSYS, and aerodynamic analysis workflows, which allows me to handle airfoil selection, dihedral optimization, CG placement, and stability validation. I can also design the airframe specifically for FDM printing. Feel free to message me in chat so I can share related UAV/mechanical design samples and discuss your concept in more detail. Thanks
$30 USD in 3 days
4.4
4.4

Hi there, A control‑surface‑free UAV relying only on differential thrust sounds simple, but the real challenge is directional stability. Without a rudder or ailerons, the aircraft must rely on dihedral, CG placement, and prop‑induced yaw/roll coupling to remain self‑correcting. If these are not balanced carefully, the aircraft either becomes uncontrollable or refuses to turn. I can design and validate a configuration where static margin, dihedral, and motor cant angles work together to produce predictable turning and natural wings‑level recovery. I have two quick questions to make sure we're on the same page: 1. Do you already have a target airfoil for low Reynolds numbers (~150k–250k), or should I select and validate one in XFLR5? 2. What motor/prop combination and thrust range are you planning, so the differential thrust authority can be modeled correctly? Let’s discuss your project now!
$90 USD in 2 days
4.1
4.1

Are you looking for a clean-sheet, stability-driven UAV airframe that is fully 3D-printable and engineered for thrust-based control? I’m a Mechanical/Electrical Design Engineer with 5+ years of experience in UAV systems, aerodynamic design, and FDM manufacturable structures. I specialize in stable, low-control aircraft concepts and CAD-to-production workflows. Approach • Aerodynamics: Airfoil + wing planform design using XFLR5 (low Reynolds optimization) • Stability: CG range, static margin, and strong dihedral for passive self-correction • Control Concept: Thrust modulation analysis (differential + total thrust behavior) • Structure: Carbon spar integration, lightweight load paths, reinforced motor mounts • Manufacturing: Modular design for 256×256 mm print bed, press-fit assembly, minimal glue • Internal Layout: CG-centered payload bay, ESC wiring channels, clean routing Deliverables • Fusion 360/STEP native CAD • Print-ready STL files (sectioned) • CG range + static margin + dihedral recommendation • Aero summary (polars, stall estimate) • Structural/material plan + print orientation guide • Assembly instructions Best Regard, Hasan
$100 USD in 3 days
3.7
3.7

As an aeronautical engineer and 3D printing specialist, I bring the perfect combination of skills needed for your project. I have extensive experience in creating precise, optimized 3D models suitable for FDM printers, including those with specific build volume constraints like your Bambu Lab printer. Moreover, my knowledge using Cura, PrusaSlicer and other slicing software helps me ensure your design is efficient and flawless. My proficiency in low Reynolds number aerodynamics will be particularly useful in enhancing the performance of your fixed-wing UAV airframe. I've also worked on projects involving structural/topology optimization, skills that would be invaluable in making your design both lightweight and sturdy. Delivering superior results has always been my forte. That's why, not only will you receive systematically organized print-ready STL files with recommended CG location and ranges, dihedral angles etc., but also detailed documented insights. These insights will include an aerodynamic analysis summary, structural recommendations and material selection per section among others. You can rely on me to give not just effective deliverables but a true asset to your project. Let’s take flight together with this unique endeavor!
$31 USD in 1 day
3.3
3.3

Hi there, I am a Mechanical Engineer with extensive experience in Fusion 360 and high-performance FDM manufacturing. I can design your stability-driven UAV, ensuring the aerodynamics and structural integrity are optimized for thrust-modulated flight. My Technical Approach: Aerodynamic Stability: I will use XFLR5 to validate the airfoil selection and define the exact dihedral angle and CG range required for inherent self-righting stability. Thrust-Vector Engineering: I’ll calculate the precise motor cant angles (upward/outward) to optimize differential thrust yaw-moments. Bambu Lab Optimized: I’ll design the airframe in 256mm sections with interlocking pins and carbon fiber spar channels for a tool-less, "press-fit" assembly. Internal Routing: Integrated channels for ESC/LED wiring and a reinforced payload bay at the CG for consistent flight behavior. Key Technical Challenges I Anticipate: Yaw Control without Rudder: Balancing motor offsets to ensure differential thrust provides enough turning force without inducing excessive roll. Stall Characteristics: Selecting a high-lift, low-speed airfoil that remains predictable at 3kg MTOW. Torsional Rigidity: Designing the wing-spar interface to handle the torque from wing-mounted tractor motors during differential thrust. Ready to start this engineering challenge immediately! Best regards, [Shahzaib]
$100 USD in 1 day
2.9
2.9

Thank you for the detailed and well-structured brief. I clearly understand the objective: a clean-sheet, inherently stable fixed-wing UAV relying exclusively on thrust vectoring (total and differential) with no conventional control surfaces. This is a challenging but very interesting design problem, especially in achieving passive stability and controllability through dihedral, CG positioning, and propulsion geometry alone. Key Technical Challenges • Achieving sufficient yaw/roll authority using only differential thrust • Ensuring strong passive roll stability without excessive drag penalty from high dihedral • Managing low Reynolds aerodynamic efficiency at this scale • Maintaining structural rigidity (especially wing) while keeping parts printable and lightweight • Balancing CG location with payload variability and motor placement I will provide complete CAD (solidworks preferred), STL files, aerodynamic analysis (polars, stability, stall), CG definition, structural recommendations, material selection, and detailed assembly/printing documentation as specified.
$250 USD in 5 days
2.5
2.5

Your emphasis on a simplicity-first, stable fixed-wing UAV without control surfaces pinpoints the real challenge: achieving reliable, self-correcting flight through thrust vectoring alone while fitting within Bambu Lab’s print constraints. Ensuring predictable stability with strong dihedral and low CG in a modular, low-part-count design is intricate but critical. I will design the airframe in Fusion 360, integrating motor mounts angled for yaw mitigation and structural channels for wiring. I will use XFLR5 for aerodynamic validation focusing on static margin and lift asymmetry effects, targeting a 3-week delivery including detailed print orientation and assembly docs. Material selection and carbon spar specs will align with load paths for minimal weight. This approach guarantees a UAV that meets your stability and manufacturability targets. What are your key priorities for balancing print complexity versus structural performance in the wing sections?
$250 USD in 7 days
2.4
2.4

With your aeronautical engineering project, I bring more than just plain CAD knowledge to the table. Having worked on various UAV, RC aircraft, and aerodynamic designs in the past, I have amassed valuable experience and a deep understanding of static stability — an essential component for your project. My proficiency with XFLR5 and CFD tools like Ansys Fluent and CFX empowers me to competently analyze and validate configurations using the low Reynolds number aerodynamics you desire. My forte in FDM design-for-manufacturing and structural/topology optimization is pivotal for a project like yours where print and load efficiencies are paramount. Moreover, my versatility with CAD software (such as SolidWorks and Fusion 360) further ensures that I can deliver the exact files you need: native CAD (preferably Fusion 360), print-ready STLs sorted by sections, CG location, recommended dihedral angle, among others. Choosing me guarantees not just the proficiency in meeting your technical requirements but also a commitment to client satisfaction that mirrors yours. I am dedicated, detail-oriented, and always ready to go that extra mile to ensure my work adds genuine value to projects; reaching targets aiming at long-term professional relationships through quality work. Let's work proactively with clear communication and understanding for a successful completion of this really fascinating project.
$35 USD in 1 day
1.7
1.7

Hi there ! With my extensive experience in 3D printing and designing for manufacturing, I believe I am tailor-made for this project. Having worked on a wide range of design projects including UAVs, I have an intimate knowledge of aerodynamic principles, low Reynolds number aerodynamics, and structural optimization that will be paramount to the success of this project. I am particularly proficient in XFLR5, CFD analysis (Ansys Fluent, CFX), and FDM design-for-manufacturing – tools that will be essential in realizing the unique challenges that your project presents. My approach to design resonates deeply with your goals - my designs are always meant to be efficient to manufacture and easy to assemble - designed not just on paper but for practical realization. With Fusion 360 as my primary tool of trade, I can guarantee you print-ready STL files along with meticulously prepared native CAD files. Intricate projects like these require a combination of skill-set and an inherent curiosity to solve problems. I believe I embody these qualities and intend to offer you not just a finished project but a comprehensive documentation that includes prints settings per part, assembly instructions, recommended material selections, and more. The world is realized by those who dare - give me the opportunity and let's dare together! Thanks & regards Gaurav sharma....
$30 USD in 2 days
0.0
0.0

Hi, As an Astronautical Engineer and Lead Engineer with a professional background in deterministic flight software and 6-DOF flight dynamics, I am uniquely prepared to design your simplicity-first, 3D-printable UAV. Why My Engineering Fits This Scope - Utilizing XFLR5 and Ansys Fluent, I will define a wing planform with the specific dihedral and static margin required. - Drawing on my work with Multi-Mode GNC and differential thrust for spacecraft recovery, I understand the accelerated lift effects necessary for turning a fixed-wing craft via motor modulation alone. - I will architect the 1.7–1.9m airframe to fit within a 256 mm bed, utilizing alignment pins and interlocking features for a "minimal-glue" assembly. I will specify the exact carbon fiber spar integration and load-path routing to ensure structural integrity at a 3 kg MTOW. Technical Challenges & Solutions - Without a rudder, the "yaw-to-roll" coupling must be precisely tuned. The primary challenge will be finding the ideal dihedral angle vs. vertical stabilizer area - Since turning relies on induced lift over the wings from the propellers, I will conduct a detailed stall estimate to ensure the craft remains controllable. - For a 3 kg aircraft, utilizing PLA for motor mounts is a risk due to ESC/motor heat. I will specify a PETG or ABS/ASA thermal strategy for the leading-edge sections to prevent structural deformation. Best regards, Batuhan Akkova
$350 USD in 10 days
0.0
0.0

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