Related Experiment Video
Updated: Aug 15, 2025

Visualization of High Speed Liquid Jet Impaction on a Moving Surface
Published on: April 17, 2015
Influence of RVGA's height on suppressing the aero-optical effects induced by a supersonic mixing layer
Abstract:
The supersonic mixing layer formed on the surface of hypersonic/supersonic flight vehicles' optical windows is the main structure that induces aero-optical effects (AOEs), which may cause severe imaging degradation. Previous research has found that the ramp vortex generator array (RVGA) with a height of 1 mm can suppress the AOE of a M c=0.17 supersonic mixing layer. In this paper, three RVGAs with different heights are considered. The nano-tracer-based planar laser scattering technique and ray tracing method are applied to do the aero-optical analysis. The root mean square of the optical path difference (O P D ), Strehl ratio (SR), imaging displacement (ID), and angle deviation (AD) are taken as evaluation parameters. It is found that a smaller aperture size (A ) corresponds to a better SR in the aperture size range of 5m m∼100m m. Then a beam with an incident angle α=15∘ and a 15 mm A is used to study the influence of RVGA's height on suppressing the AOE. When the RVGA is applied, the I D¯ and A D¯ (overline means time-averaged results) in different sections of the supersonic mixing layer are significantly normalized, which can simplify the AOE's correction procedure. The higher the RVGA is, the more the O P D ¯ is reduced and the weaker the AOE is. RVGA1 (h=1.2m m) has the best performance in suppression of the AOE because it introduces much more disturbance than RVGA2 (h=1.0m m) and RVGA3 (h=0.5m m) and achieves better inhibition of the formation and development of the K-H vortices and more reduction of the whole thickness of the supersonic mixing layer.
Related Concept Videos
Influence of Earth's Curvature and Atmospheric Refraction on Leveling
Boundary Layer Characteristics
Lift
Bernoulli's Equation for Flow Normal to a Streamline
The pressure difference depends on the fluid's velocity and radius of curvature. The pressure variation is minimal in flows with nearly straight streamlines.
Rapidly Varying Flow
Bernoulli's Equation for Flow Along a Streamline

