Over the past two decades high-fidelity simulations have become feasible for most main gas
path turbomachinery components. This paper introduces the key challenges of simulating …

View Video Presentation: https://doi. org/10.2514/6.2022-0587. vid In this work, uncertainty
in the Spalart-Allmaras (SA) turbulence model with the compressible Reynolds-averaged …

NE of the limiting factors in the design of supersonic and hypersonic vehicles remains the
prediction and control of the high aerodynamic, thermal, acoustic, and structural loads …

In this research article, three k-ε turbulence models, Standard k-ε, RNG k-ε and Realizable k-
ε were compared. The turbulent flow characteristics are illustrated in three-dimensional …

High-speed turbulent flows with shock waves pose significant challenge in terms of physical
modeling and numerical accuracy. In this paper, we develop a k-ϵ turbulence model for …

View Video Presentation: https://doi. org/10.2514/6.2021-4118. vid The shock/turbulent
boundary-layer interaction (STBLI) generated by a sharp fin with a 60 deg leading edge …

ECENT emphasis within the Department of Defense (DoD) on the development of high-
speed systems has resulted in an initiative to reinvigorate hypersonic research in the region …

In the second part of this three-paper series, high-fidelity simulations of the Transonic
Cascade TEAMAero at the aerodynamic design point with Rein= 1.35× 106 and Main= 1.21 …

One of the limiting factors in the design of supersonic and hypersonic vehicles remains the
prediction and control of the high aerodynamic, thermodynamic, acoustic, and structural …

A canonical shockwave-boundary layer interaction experiment is planned in a small working
section supersonic wind tunnel, that will allow detailed measurements of the effects of …