This paper presents an experimental study of the effect of wall cooling on the boundary-layer
structures of a sharp-nosed, 5° half-angle cone in Mach 6 flow. An experimental …

View Video Presentation: https://doi. org/10.2514/6.2022-1818. vid The shock-
wave/boundary-layer interaction that is generated by a sharp fin at incidence on a flat plate …

View Video Presentation: https://doi. org/10.2514/6.2022-1709. vid This paper presents an
extended study of the effect of cooling on the boundary-layer structures and thermal …

Measurement of the global heat flux using fast-responding temperature-sensitive paint (fast
TSP) in a shock tunnel is crucial to understanding complex aerothermal effects, but its …

Temperature-sensitive paint (TSP) is widely used to measure the temperature distribution. A
TSP is advantageous in terms of cost and spatiotemporal resolution. However, regardless of …

Measurements of the heat loads experienced by atmospheric entry spacecraft are critical to
evaluate the performance of thermal protection systems (TPS), investigate aerothermal …

Inverse heat transfer (IHT) techniques are often used to reconstruct the surface heating
conditions on spacecraft thermal protection systems (TPS) during atmospheric entry. Current …

The prediction of boundary-layer transition on hypersonic vehicles has long been
considered a primary design concern due to extreme levels of heating and dynamic …

The capability of the Temperature-Sensitive Paint (TSP) method for application in unsteady
flows in cryogenic wind tunnels was investigated by carrying out experiments in the …

Among fluid dynamic quantities measured experimentally, surface pressure and
temperature are two primary quantities that can lead to kinetics and energy acting on a fluid …