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Dhagash P.

Mechanical engineering professional

Ahmedabad, India

Global rank:

19,376 / 143,906

Skill pts: 5

Altair Hypermesh ANSYS Fluent CAD Design PTC Creo Parametric Structural Analysis

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About

Mechanical Engineering graduate with strong foundation in Computational Fluid Dynamics (CFD), Finite Element Analysis (FEA), machine and aerodynamic design. Hands-on experience in centrifugal fan optimization and industrial machinery through internships at TLT Engineering and Milacron. Led design and manufacturing teams as Vice Captain for SAE Nirma Collegiate Club, successfully competing in international SAE Aero Design competitions. Proficient in ANSYS (Fluent, Mechanical, static structure, ACP), SolidWorks, Creo Parametric, HyperMesh and advanced manufacturing techniques.

Experience

Junior Mechanical Engineer TEXEG India Private Limited · Full-time Jul 2026 – Present 1 mos GJ, India • Prepare prototypes and support new product development activities.
• Analyze mechanical and thermal test results and recommend design improvements.
Research Associate TLT Engineering India Private Limited · Internship Dec 2025 – Apr 2026 4 mos GJ, India • Evaluating existing design of centrifugal fan through computational fluid dynamics ( CFD ) and identify scope of optimization through modification of volute casing and impeller blade profile.
• Established new volute casing with 15 % weight reduction and compared it with existing design with means of
performance curve of both.
Junior Mechanical Developer Milacron Pvt. Ltd. · Internship May 2025 – Jun 2025 1 mos GJ, India • Gained experience in 3 core units : Assembly Unit | Run-off Unit | Machining Unit
• Developed understanding of machine design from both assembly and function perspectives.

Education

Nirma University Batchelor Degree in Engineering, Mechanical, 8.66/10 2022 – 2026 Activities and Societies: SAE Nirma Collegiate Club Vice Captain and Design Lead
Team Arrow, SAE Nirma Collegiate Club
Oct 2024 - Apr 2025
• Led the design and manufacturing teams for the SAE Aero Design West competition, organized by SAE International
(USA).
• Managed project parameters such as aerodynamic design, CAD modeling, structural analysis (FEA), fabrication and
flight testing for multiple models of fix-wing UAV(focusing on stability, control and payload optimization)

Other experience

Optimization of centrifugal fan Design optimization by analyzing results from CFD analysis and hands on calculation based on velocity triangle.
Aerodynamic effect of two rotating propeller of Multi-rotor UAV (Conference Paper) Conducting CFD simulations in ANSYS Workbench to analyze wake generation and evaluate aerodynamic effectiveness.
FEA(Finite Element Analysis) of composite booms Executing a project in ANSYS Composites PrepPost (ACP) to perform an in-depth analysis of composite booms within
ANSYS Mechanical Workbench.
Aerodynamic Optimization in the Design of Fixed-Wing R-C Aircraft • High-wing trailing edge tapered wing configuration was designed for caring liquid payload of up to 67 oz.
• Shoulder-wing trailing edge taper and Mid-wing Cranked dihedral wing configuration with respective payload fraction of 0.7 and 0.6.