Tariq Akilah
Project 02 / Fluid Dynamics Next / Two-Stage Avionics Bay →

Canard Roll
Control CFD


Ran 244 SimScale CFD cases for Thrust Stack, a canard-controlled airframe built for closed-loop roll stabilization, sweeping deflection from 0.55 to 9.9 degrees and freestream velocity from 33 to 113 m/s. Delivered a 162-point roll torque coefficient dataset adopted directly into the flight control logic.

Images below
Timeframe
June 2026 to August 2026
Team
Mission College, Thrust Stack, a faculty-advised 4-student research team
Role
Fluid Dynamics Research Intern
Scope
Full deflection and velocity sweep, plus a custom servo motor mount designed and manufactured to sit flush with the airframe
Tools
SimScale, SolidWorks
Status
162-point roll torque coefficient dataset delivered, adopted into the rocket's flight control logic; smaller canard geometry selected for finer control

Objective

Thrust Stack's airframe uses active canards to correct roll in flight, but the flight control team had no data on how much roll torque a given deflection actually produced at a given airspeed. Without that relationship, the controller had no way to turn a commanded correction into an actual canard angle.

The dataset had to hold up across the vehicle's full flight envelope, deflection from 0.55 to 9.9 degrees and freestream velocity from 33 to 113 m/s, since roll authority changes with both.

Approach

Built a SimScale sweep across the full deflection and velocity range, running 244 cases and about 6,200 core-hours of simulations.

The first canard geometry generated too much torque per degree of deflection for the controller to make fine corrections near small angles, so after reviewing the early sweep data, I scaled the canards down ~30% smaller than the original to trade peak torque for finer resolution. I also designed and manufactured a custom servo mount in SolidWorks, sized to sit flush with the airframe so the actuation hardware would not add parasitic drag.

Meshed CFD model of the full canard-controlled airframe
Fig. 01 / SimScale mesh, full airframe
Completed rocket airframe with nose cone, canard fin can, and static fin can labeled
Fig. 02 / Completed airframe
Servo mount CAD model
Fig. 03 / Servo mount
Servo housing CAD model
Fig. 04 / Servo housing

Result

Converted the 162-point roll torque coefficient dataset into angular acceleration using the airframe's roll moment of inertia, then delivered it to the flight control team as the lookup table the controller reads against commanded deflection and measured rocket speed.

The conversion held up cleanly to a maximum deflection of 15 degrees, which now sets the controller's usable range. The rocket is scheduled to fly in January 2027 at the Friends of Amateur Rocketry site in the Mojave Desert, California.

Chart of rotational acceleration versus vertical velocity for each canard deflection angle
Fig. 05 / Rotational acceleration vs. velocity, by deflection
SimScale pressure contour around the canard airfoil cross-section
Fig. 06 / SimScale pressure field, canard section