- 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