Registration of the Ignition of A Combustible Mixture in a Shock Tube Using a Thermoelectric Detector

Performance assessment of thermoelectric detector for heat flux measurement behind a reflected shock of low intensity

(2021) Mikhail A. Kotov et al.   APPLIED THERMAL ENGINEERING

Capabilities and limitations of existing hypersonic facilities

(2020) Sangdi Gu et al.   PROGRESS IN AEROSPACE SCIENCES

Investigation of ignition characteristics in a kerosene fueled supersonic combustor

(2019) Ye Tian et al.   ACTA ASTRONAUTICA

New insights into the shock tube ignition of H 2 /O 2 at low to moderate temperatures using high-speed end-wall imaging

(2018) Erik Ninnemann et al.   COMBUSTION AND FLAME

Advances and challenges in modeling high-speed turbulent combustion in propulsion systems

(2017) Esteban D. Gonzalez-Juez et al.   PROGRESS IN ENERGY AND COMBUSTION SCIENCE

Survey of high-enthalpy shock facilities in the perspective of radiation and chemical kinetics investigations

(2016) Philippe Reynier   PROGRESS IN AEROSPACE SCIENCES

Autoignition of propane behind shock waves

(2015) G. L. Agafonov et al.   Russian Journal of Physical Chemistry B

Recent advances in laser absorption and shock tube methods for studies of combustion chemistry

(2014) R.K. Hanson et al.   PROGRESS IN ENERGY AND COMBUSTION SCIENCE

Study of detonation initiation in kerosene–oxidizer mixtures in short tubes

(2014) J. Kindracki   SHOCK WAVES

Interpreting Endwall and Sidewall Measurements in Shock-Tube Ignition Studies

(2009) Eric L. Petersen   COMBUSTION SCIENCE AND TECHNOLOGY

Novel Sensor for Fast Heat Flux Measurements

(2009) Tim Roediger et al.   JOURNAL OF SPACECRAFT AND ROCKETS