Comparative surface heat transfer measurements in hypervelocity flow

W Flaherty, JM Austin - Journal of Thermophysics and Heat Transfer, 2011 - arc.aiaa.org
RELIABLE prediction of the high heat transfer rates experienced during the hypersonic
portion of planetary entry and descent is critical to vehicle survival. Two types of sensors that …

Assessment of heat flux on a printed scramjet inlet at Mach 7 with coaxial thermocouples in a reflected shock tunnel

LG Sgubin, LAG Ribeiro, MTA Silva… - Aerospace Science and …, 2025 - Elsevier
Measuring the thermal environment in scramjet engines is essential for develo** a high-
quality database on thermal loads, which is crucial for engine performance analysis and …

Investigation of Coaxial Surface Junction Thermocouples Under Different Materials on Thermal Measurement

L Qi, H Chen, Z Yu - Journal of Thermophysics and Heat Transfer, 2025 - arc.aiaa.org
Coaxial surface junction thermocouples (CSJTs) are commonly applied to transient thermal
measurements. Based on the measurement principle of CSJT, one-dimensional analytical …

Effects of Intrusive Probes on Incident and Reflected Regions of a Shock Tube

LA Vest, L Pitts, JC Pellegrini, I Kaltenbaugh… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
Shock tubes consistently maintain normal shock waves to produce high pressure, high
temperature environments on microsecond time scales. The University of Central Florida …

[書籍][B] Static and hypersonic experimental analysis of impulse generation in air-breathing laser-thermal propulsion

II Salvador - 2010 - search.proquest.com
The present research campaign centered on static and hypersonic experiments performed
with a two-dimensional, repetitively-pulsed (RP) laser Lightcraft model. The future …

Experimental Analysis of Heat Flux to a Blunt Body in Hypersonic Flow with Upstream Laser Energy Deposition—Preliminary Results

II Salvador, MAS Minucci, PGP Toro… - AIP Conference …, 2006 - pubs.aip.org
Due to high heat transfer rates in hypersonic flight and its consequent necessity of
prohibitively massive thermal protection system, new methods of flow control are required to …

Development of a new hypersonic shock tunnel facility to investigate electromagnetic energy addition for flow control and basic supersonic combustion

PGP Toro, MAS Minucci, JB Chanes Jr… - AIP Conference …, 2006 - pubs.aip.org
A new 0.6‐m. diameter Hypersonic Shock Tunnel is been designed, fabricated and will be
installed at the Laboratory of Aerothermodynamics and Hypersonics IEAv‐CTA, Brazil. The …

Experimental surface heat flux measurement in hypervelocity flows

WP Flaherty - 2010 - ideals.illinois.edu
Prediction of heat transfer is integral to development of hypersonic vehicles. Underprediction
of heat transfer rates can result in catastrophic failures during flight testing. An example …

Experimental Analysis of a 2‐D Lightcraft in Static and Hypersonic Conditions

II Salvador, LN Myrabo, MAS Minucci… - AIP Conference …, 2010 - pubs.aip.org
Aiming at the hypersonic phase of the Earth‐to‐Orbit trajectory for a laser propelled vehicle,
a 2‐D Lightcraft model was designed to be tested at the T3 Hypersonic Shock Tunnel at the …

Comparative study of heat flux instrumentation for hypersonic ground test facilities

TA Shams, SIA Shah, MA Ahmad… - 2018 IEEE 21st …, 2018 - ieeexplore.ieee.org
Atmospheric reentry vehicles have wing-body configuration with blunt leading edges on
wings and slender fuselage. These vehicles pass through several phases of flight during …