Combustion Zone Characterization of GO2/GH2 Rocket Using Laser-Induced Fluorescence of OH

التفاصيل البيبلوغرافية
العنوان: Combustion Zone Characterization of GO2/GH2 Rocket Using Laser-Induced Fluorescence of OH
المؤلفون: Moser, M. D, Santoro, R. J
المصدر: Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology.
بيانات النشر: United States: NASA Center for Aerospace Information (CASI), 1996.
سنة النشر: 1996
مصطلحات موضوعية: Inorganic And Physical Chemistry
الوصف: A series of studies were undertaken to measure various parameters such as velocity, species concentration, and temperature downstream of a shear coaxial injector in an optically accessible uni-element rocket chamber. Techniques applied include: laser Doppler velocimetry (LDV) for velocity; laser light scattering (LLS) for flow visualization and estimating mixture fraction and density; laser induced fluorescence (LIF) of hydroxyl radials (OH) to determine the characteristics and extent of the reaction zone; and Raman spectroscopy to measure major species concentration and temperature.
نوع الوثيقة: Report
اللغة: English
Relation: Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
URL الوصول: https://ntrs.nasa.gov/citations/19960029255
رقم الأكسشن: edsnas.19960029255
قاعدة البيانات: NASA Technical Reports