Jeffrey Lind

Jeffrey Lind

Grew AestheticOS to $130k+ annualized revenue in 3 months. Applied LLMs to civil engineering and won a $2.5m research grant. Saved PlastiExports $18,500 a year in labor. Cut a jet's avionics weight 40% and parachute cost 70%.

AestheticOS Website

AestheticOS's site is built end to end in Next.js, with hand-written WebGL fragment shaders and Motion animation sequences.

The aestheticos.ai home page: a sculpted monogram glowing over a black hero.
The website design page, splitting black typography against a cobalt engraving and live code.

Weston Center for Plastic Surgery

Full rebuild of the practice site in Next.js. Load time dropped from 7.0s to 0.6s, and 15 target keywords hit #1 on Google within weeks of launch.

The Weston Center home page: soft clinical photography under a clean, confident masthead.
The site navigation: procedure categories, patient resources, and a clear path to book.
The procedures section: surgical and non-surgical offerings laid out in a calm grid.

Lind Plastic Surgery & Med Spa

Ground-up redesign of the practice site in Next.js, spanning about 280 routes and 97,000 lines of TypeScript. 6x organic traffic and 2x lead volume vs. the prior site.

The Lind Plastic Surgery home page: refined clinical photography under a polished practice masthead.
The contact page: office details, map, and a clear path to request a consultation.
The breast augmentation procedure page: treatment overview with clinical photography and clear next steps.

DeepXFlow

Physics-informed neural net for CFD, exported to ONNX with inference running fully client-side. Basin geometry and inlet conditions are parameterized, and the velocity field re-solves in real time as they change.

DeepXFlow in the browser: geometry controls beside a velocity field across a stilling basin.
DeepXFlow architecture diagram: ONNX inference, Next.js app layer, Vercel hosting, and auth.
DeepXFlow geometry and inlet controls: depth, radius, and settling sliders on a dark sidebar.

Ψ Lab

Flume PIV and nanobubble hardware, turbine-blade testing, and talks at EURēCA 2024, CEE Seminar 2024 at UTK, and EWRI Congress 2025.

Lab team assembling a clear-channel flume: aluminum extrusions, glass walls, and hands on the frame.
Particle image velocimetry in the flume: a green laser sheet cutting through seeded flow.
Two researchers in laser-safety goggles watching a flume run under blue light.
A shop-built nanobubble generator: pump, red hoses, PVC sparger, and a glass tank.
Ψ Lab undergraduate hiring flyer: computation meets civil engineering at the Water Infrastructure Laboratory.
EURēCA 2024 research poster presenting undergraduate research work.
Presenting LLM knowledge-embedding methods at EWRI Congress 2025: podium, slide deck, and conference hall.

BMI088 Breakout Board

Bosch BMI088 IMU breakout designed in Altium and sold commercially. Its footprint is 3.8x smaller than the average competing breakout, and at $12.89 it sold for 1.4x less than the market average.

An isometric render of the BMI088 breakout: silkscreen axes, interrupt pins, and a compact IMU package.
The assembled breakout seated in a breadboard, ready for I2C bring-up.
The underside of the board, marked AeroStrike Exploration Technologies V1.0.

Eagle X

TVC rocket and extruded-aluminum launch tower with a seating pedestal and catch arms that hold and release the vehicle. Roughly 80% of components are 3D printed in PLA+ for rapid iteration and manufacturability, keeping the vehicle light. My pedestal-and-catch-arms concept predates SpaceX's use of it on Starship.

CAD of the full stack: rocket on the pad, clamp arm raised.
Top-down CAD of the pad: clamp arm, hold-downs, and the rocket seated in the ring.
Close-up of the launchpad frame: extruded aluminum, brackets, and fasteners.
The pad base from behind: hydraulic actuator, white seating ring, and black enclosure.
The Christmas rocket on the shop floor: red, white, and green airframe with a TVC fin can.
A 3D-printed thrust-vector mount cradling a motor, servos wired and ready.

Test Stand

Static-fire stand with 80 Hz load-cell thrust logging, Teensy control board, and a live thrust-curve GUI.

The stand on a hillside before a static fire, mountains and a valley town behind it.
CAD of the load-cell test stand: cube frame, motor mount, and a board labeled Got Thrust?
The controller board: a Teensy on a black carrier with screw terminals.

Project Boom

Student aircraft program focused on airframe, avionics, and recovery. As CAD and Integration Lead I cut the avionics bay weight by 40% and the parachute ejection system cost by 70%.

Project Boom aircraft strapped to a car roof under a clear sky.
Black-and-orange Project Boom airframe on display at a conference booth.
Phase-one parachute recovery system diagram: bay, shock cord, ejection charges, and sequence.