The high-thermal-conductive Carbon/Carbon (HTC-C/C) composites using mesophase-pitch-
based carbon fibers (CF MP) as heat conduction carriers are promising thermal …

By slotting an inlet at the head of the aerodisk, a channel through the spike, and the lateral
jet outlet at the middle of the spike, the blunt body with spike-aerodisk can further reduce its …

As for blunt-body hypersonic vehicles, the extreme drag and aero-heating pose great
challenges to the conceptual design. Different from the conventional configurations, a blunt …

Aerodynamic heating and impact resistance present significant challenges for hypersonic
aircraft. This study introduces a novel multi-jet strategy to enhance both resistance reduction …

Among the design requirements of hypersonic vehicles, reducing aerodynamic heating and
drag force simultaneously is the main challenge. This paper proposes a novel spike …

When an aircraft flies at hypersonic speeds, a large aerodynamic drag and a significant
amount of aerodynamic heat are generated around it. As an active flow control technology …

Thermal insulation structure is a key factor to protect a high-speed aircraft to work safely and
complete various tasks. The multilayer thermal insulation (MTI) structure has attracted much …

Joule heating is a useful experimental technique for ground based hypersonic testing as it
allows replication of the governing wall-to-freestream temperature ratio and thus better …

The structural integrity of sapphire optical windows was numerically and experimentally
evaluated under the wall heat flux of the scramjet intake. The considered heating profile was …

View Video Presentation: https://doi. org/10.2514/6.2022-3796. vid This work aims to
develop a cost-efficient experimental technique for studying fluid-thermal-structural …