Also from GTL
ZeusHydrogen HALE · stratospheric 5G
NautilusReusable SSTO launch vehicle
RDRERotating detonation rocket engine
GTL GTL Gloyer-Taylor Laboratories
What We Do · Modeling & Simulation

Modeling &
simulation

GTL's analysis capability is the foundation under its hardware — predicting combustion stability and coupled physics before anything is built, so engines and structures are designed right the first time.

UCDS
Combustion-stability model
40+ yrs
Combustion-instability research
Multiphysics
Coupled analysis
SimDAT
Simulation data tooling
/ 01 — Combustion Stability

The UCDS model, decades in the making.

GTL's Universal Combustion Device Stability (UCDS) model — rooted in Chief Engineer Dr. Gary Flandro's 40+ years of combustion-instability research — provides an unprecedented ability to accurately predict the stability of steady-flow combustion devices. Dr. Josh Batterson and Dr. Eric Jacob have continued Dr. Flandro's work, extending UCDS to include full multi-physics numerical simulation, nonlinear wave-steepening, and CFD CI post processing analysis.

Rather than discovering instability on the test stand, UCDS lets GTL design in a high stability margin from the outset — the insight behind the Superior Stability Engine.

/ 02 — Multiphysics Modeling

Coupled analysis across fluids, structures, and thermal.

GTL applies coupled multiphysics modeling — fluid dynamics, structural, and thermal analysis — to aerospace systems operating in extreme environments, from cryogenic tankage to high-temperature propulsion, linking the physics that conventional single-discipline tools treat in isolation.

This work is led by Dr. Josh Batterson, GTL's Director of Modeling & Simulation, whose custom multiphysics framework couples a compressible reacting-flow CFD solver with conjugate heat transfer, acoustics, and structural mechanics — spanning acoustic, vorticity, thermal, and hydrodynamic wave solvers, genetic algorithms, smoothed-particle hydrodynamics, and structural mechanics.

Schlieren-style density field of acoustic waves radiating from a transonic cavity
Acoustic waves in a transonic cavity
Measured density vs. computed density of sound reflection in a gap
Sound reflection in a gap — measured vs. computed density
Pressure field simulation of baffled sound radiation
Baffled-sound simulation — radiated pressure field
Detonation model showing pressure (p) and chemical-source (H) fields in a channel
Detonation model — pressure and reaction fields
/ 03 — SimDAT

Seeing the instability, mode by mode.

SimDAT is GTL's simulation data-analysis toolset. Starting from the unsteady flow field, it decomposes the solution into individual acoustic and hydrodynamic modes, then localizes where sound is generated — isolating the vortex-shedding and heat-release sources that drive combustion instability. This methodology is detailed in our AIAA-JPP publication.

Unsteady density field evolving in the combustor over time
Unsteady field — the raw time-resolved simulation
First longitudinal (L1) acoustic density mode extracted from the unsteady field
Example decomposition — extracted ρ L1 acoustic mode
Rayleigh sound-generation field from vortex shedding along the combustor
SOUND GENERATION FROM VORTEX SHEDDING - BLUE = SOUND DRIVING - ORANGE = SOUND DAMPING
Rayleigh sound-generation field from unsteady heat release
Sound generation from unsteady heat release - BLUE = SOUND DRIVINg - ORANGE = SOUND DAMPING
* UNSTEADY CFD PROVIDED BY PURDUE UNIVERSITY