Peculiarities of Ramjet Combustion Chamber Work with Resonator Under Condition of Vibration Fuel Combustion
Abstract
An optical measurement and registration system of electronic radiation of electron-excited radicals OH in flames is presented in this work. To investigate diffusion hydrogen-air torches the mentioned system was used. The obtained experimental data were used for analysis of a thrust formation of the ramjet ejector combustor with acoustic resonator by vibrating burning of hydrogen. It was offered a way to determine geometrical parameters of ejector system and hydrogen consumptions providing the largest thrust values.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 2002
- Accession Number
- ADA409132
Entities
People
- A. A. Pavlov
- A. V. Potapkin
- D. Yu. Moskvichev
Organizations
- Russian Academy of Sciences