Plif imaging measurements of a co-axial rocket injector spray at elevated pressure

Symposium (International) on Combustion

Volumn 26, Issue 1, 1996, Pages 1687-1695

  Brummund, U ^a   Cessou, A ^a   Vogel, A ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ATOMIZATION; COMBUSTION CHAMBERS; FLUORESCENCE; FUEL INJECTION; HIGH PRESSURE EFFECTS; HYDROGEN; IMAGING TECHNIQUES; LASER DIAGNOSTICS; LIQUID FUELS; OXYGEN; PROPELLANTS; TWO PHASE FLOW;

CO AXIAL ROCKET INJECTOR; ELEVATED PRESSURE; PLANAR LASER INDUCED PREDISSOCIATION FLUORESCENCE; TURBULENT MIXING;

COMBUSTION;

EID: 0030349641     PISSN: 00820784     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0082-0784(96)80393-6     Document Type: Article

References (18)

1. AIAA 95-0141, 33rd Aerospace Sciences Meeting and Exhibit
2. Predissociation lifetimes of OH A 2Σ+ (v’=3) obtained from optical–optical double-resonance linewidth measurements
3. Laser-induced fluorescence with tunable excimer lasers as a possible method for instantaneous temperature field measurements at high pressures: checks with an atmospheric flame
4. Absolute Temperature Fields in Flames by 2D-LIF of OH Using Excimer Lasers and CARS Spectroscopy