Simulation of multistage compressor at off-design conditions

F Wang, M Carnevale… - Journal of …, 2018 - asmedigitalcollection.asme.org
Computational fluid dynamics (CFD) has been widely used for compressor design, yet the
prediction of performance and stage matching for multistage, high-speed machines remains …

Virtual gas turbine: Pre-processing and numerical simulations

F Wang, M Carnevale, G Lu… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
The design process of a gas turbine engine involves interrelated multi-disciplinary and multi-
fidelity designs of engine components. Traditional component-based design process is not …

Lip stall suppression in powered intakes

M Carnevale, F Wang, JS Green… - Journal of Propulsion and …, 2016 - arc.aiaa.org
This work describes a computational study into lip stall in subsonic civil aircraft intakes and
its alleviation by action of the fan. Beyond a certain flow incidence, the lower lip of a civil …

Low frequency distortion in civil aero-engine intake

M Carnevale, F Wang… - … of Engineering for …, 2017 - asmedigitalcollection.asme.org
The main role of the intake is to provide a sufficient mass flow to the engine face and a
sufficient flow homogeneity to the fan. Intake-fan interaction off design represents a critical …

Virtual Gas Turbines part II: an automated whole-engine secondary air system model generation

D Kulkarni, L di Mare - Journal of Engineering for …, 2022 - asmedigitalcollection.asme.org
The design and analysis of the secondary air system (SAS) of gas turbine engine is a
complex and time-consuming process because of the complicated topology and iterative …

Fluid Dynamics of Turbine Rim Seal Structures: A Physical Interpretation Using URANS

G De Cosmo, JA Scobie… - … for Gas Turbines …, 2023 - asmedigitalcollection.asme.org
Abstract Unsteady Reynolds-averaged Navier–Stokes modeling (URANS) is a valuable and
cost-effective tool for computational fluid dynamics (CFD), including the investigation of …

Mesh generation for turbomachinery blade passages with three-dimensional endwall features

F Wang, L di Mare - Journal of Propulsion and Power, 2017 - arc.aiaa.org
Turbomachinery blade passages are conventionally meshed by sweeping a mesh from a
reference stream surface to other stream surfaces along the blade span. This approach is …

Analysis of transonic bladerows with non-uniform geometry using the spectral method

F Wang, L di Mare - Journal of Turbomachinery, 2021 - asmedigitalcollection.asme.org
Turbomachinery blade rows can have non-uniform geometries due to design intent,
manufacture errors or wear. When predictions are sought for the effect of such non …

Favre-averaged nonlinear harmonic method for compressible periodic flows

F Wang, L di Mare - AIAA Journal, 2019 - arc.aiaa.org
The treatment of compressible flows subject to periodic disturbances of finite amplitude with
nonlinear harmonic (NLH) methods requires a careful choice of averaging procedures and …

Software prefetching for unstructured mesh applications

I Hadade, TM Jones, F Wang, L Mare - ACM Transactions on Parallel …, 2020 - dl.acm.org
This article demonstrates the utility and implementation of software prefetching in an
unstructured finite volume computational fluid dynamics code of representative size and …