I. Introduction nder the Test Resource Management Center (TRMC) and Air Force Office of
Scientific Research (AFOSR) funded Hypersonic Center of Testing Excellence (CoTE), the …

This paper compares the calibration of different heat flux sensors in radiation-and
convection-based sub-and supersonic operation. First, four heat flux sensors based on …

In this paper, we report on the application of the atomic layer thermopile (ALTP) heat-flux
sensor to the measurement of laminar-to-turbulent transition in a hypersonic flat-plate …

The goal of the Hypersonic Integrated Flight Research and Experimentation (HIFLIER) flight
experiment was to measure second-mode boundary-layer instabilities and subsequent …

A new flight experiment was designed and flown with the goal of measuring second-mode
boundary-layer instabilities and subsequent transition in atmospheric flight at hypersonic …

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 …

In this study a fast-response Atomic Layer Thermopile (ALTP) based heat flux measurement
system is used for wall heat-flux determination in the combustion chamber of a commercially …

高超声速边界层转捩对摩阻, 传热等有重要影响, 飞行器的研制迫切希望能精确预测和控制边界
层转捩. 在JF8A 激波风洞中开展了7 半锥角的高超声速尖锥边界层转捩实验研究 …

In this study, the static calibration of different heat flux sensors in radiation-and convection-
based procedures are compared. First, three heat flux sensors based on different principles …

We present measurements of fluctuating heat flux in a turbulent, incident shock/boundary-
layer interaction (SBLI) at Ma= 2.0 using fast-response ALTP (Atomic Layer Thermo Pile) …