Response of second-mode instability to backward-facing steps in a high-speed flow

G Gong, G Tu, B Wan, C Li, J Chen, W Hu - Physics of Fluids, 2024 - pubs.aip.org
Stability in a Mach 4.5 boundary layer over backward-facing steps (BFSs) is investigated
using numerical methods. Two types of cases are considered with different laminar inflow …

[HTML][HTML] Research progress of aero-optical effect

SUN Xiwan, LIU Wei - 力学进展, 2020 - lxjz.cstam.org.cn
Optical imaging detection is an important research direction in the precision guide field. The
quality of observation would be profoundly deteriorated due to the aberration, jitter, and …

Improving the aerodynamic performance of wig aircraft with a micro-vortex generator (mvg) in low-speed condition

Z Methal, ASA Talib, MSA Bakar, MRA Rahman… - Aerospace, 2023 - mdpi.com
This present study investigated the potential of passive flow control to reduce induced drag
by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location. A wing-in …

Potential of micro-vortex generators in enhancing the quality of flow in a hypersonic inlet-isolator

AC Idris, MR Saad, K Kontis - Journal of Advanced Research …, 2021 - semarakilmu.com.my
The rush to be the first to demonstrate a practical hypersonic cruise missile has never been
more frantic among the world's superpowers, especially since China and India have also …

[PDF][PDF] Numerical Forced Convection Heat Transfer of Nanofluids over Back Facing Step and Through Heated Circular Grooves.

AH Abdulkarim, MA Eleiwi, TA Tahseen… - Mathematical Modelling …, 2021 - researchgate.net
Accepted: 11 June 2021 Backward facing step arrangement is a classical case for fluid
dynamics and heat transfer research. It is well characterized and therefore, used for …

Inhibition of the aero-optical effects of supersonic mixing layers based on the RVGAs' control

Z Xia, H Ding, S Yi - Chinese Optics Letters, 2023 - opg.optica.org
The infrared imaging windows of the hyper/supersonic optical dome are encountering
severe aero-optical effects (AOEs), so a flow control device, the ramp vortex generator array …

Dynamics and spectral character of unsteady pressure field on afterbody of generic space launcher: Transonic flows

NS Vikramaditya, M Viji - European Journal of Mechanics-B/Fluids, 2024 - Elsevier
The unsteady pressure field over an axisymmetric backward-facing step was investigated
experimentally at transonic freestream Mach numbers of 1.05, 1.2, and 1.4. The study was …

Experimental study on the influence of attitude angle on the aero-optical effects of a hypersonic optical dome

X Zhao, S Yi, H Ding - Optik, 2020 - Elsevier
The aero-optical effects of a hypersonic dome with cooling jet device can be mitigated by
micro vortex generators (MVGs) at 0° angle of attack (AoA) and 0° angle of sideslip (AoS) …

[HTML][HTML] 气动光学效应研究进展

孙喜万, 刘伟 - 力学进展, 2020 - lxjz.cstam.org.cn
光学成像探测技术是精确制导领域发展的重要方向, 但由于光线在穿过密度变化的流场时会发生
偏折, 抖动和光程变化的现象, 成像质量将严重下降, 此即气动光学效应. 研究气动光学效应同时 …

Aero-optical suppression for supersonic turbulent boundary layer

X Sun, XL Yang, W Liu - Journal of Turbulence, 2021 - Taylor & Francis
Aero-optical reduction in flat-plate turbulent boundary layer has been widely concerned due
to critical application for high-speed target-seeking vehicles. From the perspective of …