SU2: An open-source suite for multiphysics simulation and design

TD Economon, F Palacios, SR Copeland, TW Lukaczyk… - Aiaa Journal, 2016 - arc.aiaa.org
This paper presents the main objectives and a description of the SU2 suite, including the
novel software architecture and open-source software engineering strategy. SU2 is a …

Adjoint methods as design tools in thermoacoustics

L Magri - Applied Mechanics Reviews, 2019 - asmedigitalcollection.asme.org
In a thermoacoustic system, such as a flame in a combustor, heat release oscillations couple
with acoustic pressure oscillations. If the heat release is sufficiently in phase with the …

Discrete Empirical Interpolation Based Hyper-Reduced Order Model for Steady Hypersonic Flows

SS Joshi, R Prasad, S Choi - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0079. vid Hypersonic vehicle
design has traditionally relied upon correlation-based models and low-to medium-fidelity …

[PDF][PDF] Adjoint-based aerodynamic design optimisation in hypersonic flow

KA Damm - 2020 - core.ac.uk
The drive for improved flexibility and reusability in satellite launch systems has brought a
resurgence in the popularity of scramjet-powered access-to-space launch vehicle concepts …

[图书][B] A Discrete Adjoint Framework for Turbulent Hypersonic Flows in Thermochemical Nonequilibrium

WT Maier - 2023 - search.proquest.com
Hypersonic vehicle design and analysis continues to challenge the aerospace community.
These systems operate in a unique flow environment characterized by thermochemical …

Aero-Thermo-Elastic Sensitivity Analysis of a Scramjet Inlet

J Horing, K Maute, ID Boyd - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
At hypersonic speeds, fluid-thermal-structural interactions (FTSI) can create unexpected
changes to a vehicle's behavior. Geometries such as scramjet inlets, which are highly …

Sensitivity-Based Parameterization for Aerodynamic Shape Global Optimization

H Li, C Li, W Chen, H Yang - Journal of Aerospace Engineering, 2022 - ascelibrary.org
For aerodynamic shape design using gradient-free searching algorithms, which can be
applied more flexibly than gradient-based ones, computing costs increase dramatically with …

[图书][B] Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation

KB Thompson - 2017 - search.proquest.com
An algorithm is described to efficiently compute aerothermodynamic design sensitivities
using a decoupled variable set. In a conventional approach to computing design sensitivities …

[PDF][PDF] Refinement of Design Variables for Aerodynamic Shape Optimization

H Li, Z Guo, W Chen - iccfd.org
To investigate the impact of distribution of design variables on global optimization design, a
determination strategy of variables and corresponding design space adjustment method …

[引用][C] 高速组合体布局飞行器外形快速优化方法研究

张宇飞, 尘军, 邓帆, 付秋军, 杜新 - 战术导弹技术, 2016