High-temperature thin film heat flux sensors have been fabricated by growing c-axis tilted
epitaxial Ca 3 Co 4 O 9 (CCO) thin films on 5 vicinal cut LaAlO 3 (001) single crystal …

The development of well-characterized, reliable, and cost-effective platforms for
experimental aerothermodynamic research is a key factor to advance hypersonic …

Traditional contact heat flux sensors suffer from a lack of dynamic performance, and existing
non-contact optical heat measurement equipment fails to detect convective heat transfer …

The atomic layer thermopile (ALTP) heat flux sensor has played an important role in the
study of boundary layer transition. However, the response characteristics of the sensors still …

Measuring the heat-flux density is one of the main tasks in the research field of hypersonic
experimental aerodynamics. Considering the fact that refined wind tunnel tests require small …

Venturi flow meters are pressure differential devices that perform accurate measurements
with minimal pressure losses. They are widely used and well-documented in high-Reynolds …

The influence of various parameters on the laminar-turbulent transition of hypersonic
boundary layers is a subject of ongoing investigation. This study aims to utilize a new …

Heat flux is an important parameter to be considered for the field of the optimization of
thermal protection to maintain the hot-end component's long lifetime and stability under …

Abstract The Transverse Seebeck Effect (TSE) in a 20° inclined epitaxial nitrogen-doped 4H-
SiC thin film was observed for the first time. When excited by a 248 nm pulsed laser with a …

Forward-facing cavities (FFC's) have been characterized in hypersonic quiet-flow at Angles-
of-Attack (AoA's) utilizing Purdue University's Boeing/AFOSR Mach 6 Quiet Tunnel …