Fast and reliable prediction of scramjet flowfields via Gaussian process latent variable model and deep learning

• Published in: Physics of fluids (1994) Vol. 35; no. 4
• Main Authors: Fujio, Chihiro, Akiyama, Kento, Ogawa, Hideaki
• Format: Journal Article
• Language: English
• Published: Melville American Institute of Physics 01.04.2023
• Subjects: Deep learning; Fluid dynamics; Fuel injection; Gaussian process; Machine learning; Physics; Prediction models; Predictions; Reduced order models; Reliability; Supersonic aircraft; Supersonic combustion ramjet engines
• ISSN: 1070-6631; 1089-7666
• DOI: 10.1063/5.0148974

Fast and accurate prediction of high-speed flowfields is of particular interest to researchers in fluid science and engineering to enable efficient design exploration and knowledge discovery. The reliability of prediction is another important metric for the performance of prediction models. While predictive modeling approaches with and without reduced-order modeling (ROM) via machine learning techniques have been proposed, they are inherently subject to loss of information for ROM-based approaches and substantial computational costs in modeling for non-ROM-based approaches. This paper proposes an accurate ROM-based predictive framework with minimum information loss enabled by incorporating Gaussian process latent variable modeling (GPLVM) and deep learning. The stochastic nature of GPLVM allows for uncertainty quantification that indicates the degree of prediction error or reliability of prediction without requiring validation data. The applicability for supersonic/hypersonic viscous flowfields has been examined for two cases including axisymmetric intakes and two-dimensional fuel injection in scramjet engines by comparison with other predictive models. Comparable or superior prediction accuracy over the other models has been achieved by the proposed approaches, demonstrating its high potential to serve as a new competent, data-driven technique for fast, accurate, and reliable prediction of scramjet flowfields.