- Author
- Oschwald, M. | Smith, J. J. | Branam, R. | Hussong, J. | Schik, A. | Chehroudi, B. | Talley, D.
- Title
- Injection of Fluids Into Supercritical Environments.
- Coporate
- German Aerospace Center (DLR), Lampoldshausen, Germany Engineering Research Consultants, Lancaster, PA U.S. Air Force Research Laboratory (AFRL), Edwards Air Force Base, CA
- Journal
- Combustion Science and Technology, Vol. 178, No. 1-3, 49-100, January/March 2006
- Keywords
- fluids | injection | sprays | pressure | cryogenic liquids | nitrogen | temperature | combustion | high pressure | thermophysical properties | experiments | equations | mapping | simulation | temperature fields | hydrogen | density effects | fire tests | propellants | rocket engines | combustion chambers | oxygen | fractals | fractal analysis | liquid nitrogen
- Identifiers
- injection of cryogenic liquids at subcritical and supercritical pressures; shadowgraphy and spontaneous Raman scattering; combustion chamber pressure of LOX/H2 engines in units of the critical pressure of oxygen; critical properties of relevant fluids; AFRL test bench; DLR cryo-injector test bench; DLH high-pressure combustion test bench P8; single-jet investigations; phenomenology at subcritical and supercritical pressures; length scale analysis; jet decay; visualization of jet core length; jet spreading angles; phenomenological model of the jet growth rate