Combustion Simulation Under Variable Pressure Conditions

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Solution Overview

Problem

Current computer graphics methods struggle to accurately and efficiently simulate large-scale combustion events and cloud formation, leading to unrealistic visual representations due to the computational intensity of fully compressible atmospheres, which are necessary for realistic modeling but prohibitive in terms of computational power.

Innovation Solution

A computationally efficient method is developed to simulate combustion and cloud formation using continuum mechanics equations that account for conservation of momentum and mass, with the option to treat combustion products as either incompressible or compressible, and employing a convolution kernel for heat diffusion, allowing for visually convincing results with reduced computational overhead.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If fully compressible atmosphere models are used for large-scale combustion simulation, then visual realism is improved, but computational power requirements become prohibitive

Engineering Contradiction:
Improvevisual realismVSAvoidcomputational power
Core Design Contradiction:
Manufacturing precisionVSUse of energy by moving object

Solution Approach 1:

The atmosphere is segmented into two distinct regions: an incompressible lower atmosphere where combustion occurs, and a compressible upper atmosphere that handles adiabatic expansion. This segmentation allows the simulation to use computationally efficient incompressible flow equations for the majority of the combustion process while only applying complex compressible physics where absolutely necessary for visual realism during expansion phases.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies compressible atmosphere modeling only partially - specifically for the upper atmosphere region during adiabatic expansion phases - rather than throughout the entire simulation. This partial application provides sufficient visual realism for large-scale combustion events while avoiding the prohibitive computational cost of fully compressible models.

Inventive Principle:
Principle #16Partial or excessive action

2Productivity

If incompressible atmosphere models are used, then computational efficiency is improved, but visual realism of large-scale combustion events deteriorates

Engineering Contradiction:
Improvecomputational efficiencyVSAvoidvisual realism
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The patent dynamically changes the compressibility parameter of the atmosphere based on the simulation phase and spatial location. During combustion phases in the lower atmosphere, the model treats the gas as incompressible (constant density). During adiabatic expansion phases in the upper atmosphere, the model transitions to compressible behavior where density varies with pressure and temperature, thereby achieving visual realism when needed while maintaining computational efficiency during combustion phases.

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If compressible fluid equations are used for combustion simulation, then accuracy of large-scale phenomena is improved, but computational complexity increases

Engineering Contradiction:
Improveaccuracy of large-scale phenomenaVSAvoidcomputational complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The computational domain is segmented vertically into a lower incompressible region and an upper compressible region. This spatial segmentation allows the use of simpler incompressible Navier-Stokes equations for the combustion zone while applying full compressible thermodynamic equations only in the upper atmosphere where adiabatic expansion occurs, thereby reducing overall computational complexity while maintaining accuracy for large-scale phenomena.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The model dynamically switches between incompressible and compressible fluid equations based on the simulation phase and spatial location. During combustion phases, incompressible equations are used; during expansion phases, compressible equations are activated. This dynamic adaptation reduces computational complexity by avoiding unnecessary use of complex compressible equations when simpler models suffice.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach enhances the realism of simulations by accurately modeling large-scale combustion and cloud formation without the need for full compressibility, achieving realistic visual representations with minimal additional computational time compared to incompressible atmosphere models.

Implementation Method 1

a visualization of combustion, such as a movie action scene wherein something combusts

Methodology Applied
Scientific EffectCombustion: Combustion

Implementation Method 2

combustion event, which transforms combustion reactants into combustion products

Methodology Applied
Scientific EffectExothermic reaction: Exothermic Reaction

Implementation Method 3

employing a convolution kernel for heat diffusion

Methodology Applied
Scientific EffectHeat diffusion: Conduction (thermal)

Implementation Method 4

convert a room-temperature solid, liquid, or gas into an expanding cloud of hot reaction products

Methodology Applied
Scientific EffectAdiabatic expansion: Adiabatic Heating

Data Source

PatentUS11475621B2Method for simulating combustion in digital imagery with variable pressure conditions
Publication Date: 2022.10.18 UNITY TECH SF
  • US11475621B2 patent drawing
  • US11475621B2 patent drawing
  • US11475621B2 patent drawing

AI summary

A computer-implemented method simulates an atmospheric phenomenon within a simulation volume. At each time step of a plurality of time steps, the method automatically determines a temperature distribution of the atmospheric phenomenon based on an assumption of fixed volume, and then automatically determines a velocity field of the atmospheric phenomenon, based on an assumption of adiabatic expansion.