Aerospace PhD candidate at Stanford. Uncertainty quantification for machine learning, applied to aircraft design.
The jam happened at the moment of engagement, so I removed the engagement.
Asked everyone what annoyed them about the old one, then reproduced every complaint myself before believing it.
Most of the drag was frontal area, and the only thing stopping me cutting it was the driver's eyeline.
The shell was sagging at competition. Stiffening it was not going to happen that weekend, so I carried the load somewhere else.
Type an address into a browser; the aircraft flies there.
Reasoned from the lift equation: if you cannot change density or angle of attack, change the wing.
| drawn | A. SHAH |
| subject | SELECTED WORK |
| sheet | 1 of 1 |
| views | 7 |
| date | 2026-10-07 |
| rev | 6666FD2 |