UNIVERSITY OF FLORIDA · AEROSPACE & MECHANICAL ENGINEERING

Chase Turmail.

Mechanical Design • Aerospace Analysis

Seeking Summer 2027 Engineering Internships

I redesigned and assembled a precision collimator prototype during an internship, then brought the same systems approach to propulsion CAD and UAV analysis.

EDUCATIONDual B.S.

Aerospace + Mechanical Engineering · UF

ACADEMIC RECORD3.92 / 4.00

Dean’s List every semester

CURRENT ROLEMechanical Engineering Intern

Imaging Engineering · Prototype 1 design + assembly

SELECTED ENGINEERING WORK

Hardware. Propulsion. Aerodynamics.03

Three case studies showing my role, design decisions, evidence, and current status.

Overall view of the completed physical Prototype 1 assembly with linear actuators, linear guides, custom mounts, and 3D-printed structural components.
01 / MECHANICAL DESIGN / INTERNSHIPPrototype 1 physically assembled
Designed + Physically Assembled

Precision Collimator Prototype

I independently redesigned the mechanism in Fusion 360, integrated linear motion hardware, custom mounts, and 3D-printed structure, and assembled Prototype 1. Performance testing is not claimed.

RECRUITER SNAPSHOT
Role
Independent redesign + assembly
Decisions
Motion integration + interfaces
Evidence
Physical Prototype 1
Fusion 360Electromechanical integrationPrototype assembly
View Case Study
Open-casing conceptual turbojet CAD assembly showing the compressor, combustor, turbine, and support stand.
02 / PROPULSION / MECHANICAL DESIGNConceptual, non-running design · prototyping next
Calculated + Designed

Axial-Flow Turbojet

About 300 hours of independent sizing, CAD, and mechanical integration. The 1,000 N thrust figure is a target; the preliminary shaft-power match is calculated, not measured.

RECRUITER SNAPSHOT
Thrust
1,000 N design target
Airflow
≈ 1.91 kg/s modeled requirement
Power balance
≈ 213.8 kW preliminary match
Preliminary sizingSolidWorksMechanical integration
View Case Study
XFLR5 lifting-surface model of the final electric UAV configuration with SD7037 wing, NACA 0012 tail surfaces, dihedral, and tip twist.
03 / AERODYNAMICS / STABILITYXFLR5 analysis complete · prototype not yet flown
Analyzed + Designed

Stable Electric UAV

XFLR5 and MATLAB study of a 5.0 kg electric UAV, including wing sizing, airfoil trades, trim, and predicted stability. No flight test yet.

RECRUITER SNAPSHOT
Design point
5.0 kg at 18 m/s
XFLR5 prediction
L/D 24.18
XFLR5 prediction
10.4% static margin
XFLR5 / XFoilMATLABStability analysis
View Case Study
Completed Imaging Engineering Prototype 1 assembly with linear actuators, linear guides, custom mounts, and 3D-printed structure.
Imaging Engineering · Prototype 1 physical assembly

ENGINEERING EXPERIENCE

Designed + Physically Assembled

A redesign carried into real hardware.

As a Mechanical Engineering Intern at Imaging Engineering, I independently redesigned a precision collimator mechanism in Fusion 360 and assembled Prototype 1.

  • Integrated linear actuators and guides with custom mounts and 3D-printed structural parts.
  • Designed metric fastener, clearance, and tapped interfaces; refined component placement during assembly.
  • Completed the first physical assembly. Measured performance and production validation are not claimed.
View Prototype 1 Case Study

TECHNICAL TOOLKIT

Tools used in the work.

SolidWorks CSWA • Fusion 360 • MATLAB • XFLR5 • CAD • Mechanical Design • Aerodynamics • Prototyping

CURRENTLY

Building depth across aerospace and mechanical systems.

Mechanical Engineering Intern at Imaging Engineering • Developing independent turbojet and UAV projects • Seeking Summer 2027 aerospace and mechanical engineering opportunities.

I’m pursuing dual bachelor’s degrees in aerospace and mechanical engineering at the University of Florida, with expected graduation in December 2027. My long-term interests include rockets, satellites, spacecraft, and the mechanical systems that make them work.

RESUME + CONTACT

Let’s talk engineering.

Available for Summer 2027 aerospace and mechanical engineering internship opportunities.