[HTML][HTML] Retro-propulsion in rocket systems: Recent advancements and challenges for the prediction of aerodynamic characteristics and thermal loads

T Bykerk, S Karl, M Laureti, M Ertl, T Ecker - Progress in Aerospace …, 2024 - Elsevier
This paper presents a review of recent literature on the application of retro-propulsion in
earth based rocket systems, with a specific focus on the recent advancements and …

Anisotropic SST turbulence model for shock-boundary layer interaction

P Raje, K Sinha - Computers & Fluids, 2021 - Elsevier
Menter SST k-ω is a Reynolds-averaged Navier–Stokes based two-equation turbulence
model routinely used in industry for predicting aerodynamic flows. It shows excellent …

Numerical simulation of scramjet engine with compressibility corrections on k-εmodel based on OpenFOAM

W Zhang, X Zheng, P Yan, R Xue - International Communications in Heat …, 2024 - Elsevier
Supersonic flows exhibit compressible effects and ignoring this influence would lead
deviations in supersonic combustion simulation. In this study, taking the standard k− ε …

[HTML][HTML] Bayesian parameter estimation of SST model for shock wave-boundary layer interaction flows with different strengths

T Denggao, LI Jinping, Z Fanzhi, LI Yao… - Chinese Journal of …, 2023 - Elsevier
Abstract The Shock Wave-Boundary Layer Interaction (SWBLI) flow generated by
compression corner widely occurs in engineering. As one of the primary methods in …

Studies on sootblower jet dynamics and ash deposit removal in industrial boilers

A Pophali, B Emami, M Bussmann, H Tran - Fuel processing technology, 2013 - Elsevier
Sootblowers used to control deposit accumulation on boiler tubes consume substantial
amounts of costly high pressure steam; this cost motivates the study of sootblowers and …

Modeling structural uncertainties in Reynolds-averaged computations of shock/boundary layer interactions

M Emory, R Pecnik, G Iaccarino - … including the new horizons forum and …, 2011 - arc.aiaa.org
Computational fluid dynamics (CFD) is widely used by engineers in a range of applications,
providing a wealth of information about the flow characteristics. Despite this ability to …

Padé–Legendre approximants for uncertainty analysis with discontinuous response surfaces

T Chantrasmi, A Doostan, G Iaccarino - Journal of Computational Physics, 2009 - Elsevier
A novel uncertainty propagation method for problems characterized by highly non-linear or
discontinuous system responses is presented. The approach is based on a Padé–Legendre …

Interplay of surface deformation and shock-induced separation in shock/boundary-layer interactions

KR Brouwer, A Gogulapati, JJ McNamara - AIAA Journal, 2017 - arc.aiaa.org
Shock wave/boundary-layer interactions represent an extreme loading condition in the
structural design of high-speed flight vehicles. However, the complexity of this problem has …

Turbulent energy flux generated by shock/homogeneous-turbulence interaction

R Quadros, K Sinha, J Larsson - Journal of Fluid Mechanics, 2016 - cambridge.org
High-speed turbulent flows with shock waves are characterized by high localized surface
heat transfer rates. Computational predictions are often inaccurate due to the limitations in …

Ground test studies of the HIFiRE-1 transition experiment Part 2: computational analysis

M MacLean, T Wadhams, M Holden… - Journal of Spacecraft and …, 2008 - arc.aiaa.org
FULLY duplicated ground test experiments have been performed in the CUBRC (Calspan–
University at Buffalo Research Center) LENS I shock-tunnel facility to develop and validate …