|
Volumn 3172, Issue , 1997, Pages 506-
|
Improved optical techniques for studying sonic and supersonic injection into Mach 3 flow
|
Author keywords
[No Author keywords available]
|
Indexed keywords
ABSORPTION CELLS;
AIR INJECTIONS;
CAMERA SYSTEMS;
CONTINUOUS FLOWS;
FILTERED RAYLEIGH SCATTERINGS;
HIGH SPEEDS;
INJECTANT;
LASER LIGHTS;
LIQUID OXYGENS;
MOIST AIRS;
ND:YAG PULSED LASERS;
NUCLEAR THERMAL ROCKETS;
OPTICAL TECHNIQUES;
RAYLEIGH;
SCATTERED LIGHTS;
STATIC PRESSURE DATUMS;
SUPERSONIC INJECTIONS;
SUPERSONIC WIND TUNNELS;
TRANSVERSE SECTIONS;
VARIOUS CONFIGURATIONS;
VISUALIZATION IMAGES;
CAMERAS;
CHARGE COUPLED DEVICES;
COMBUSTION;
FLOORS;
FLOW VISUALIZATION;
FLUID DYNAMICS;
HELIUM;
INERT GASES;
IODINE;
JET PUMPS;
LIQUEFIED GASES;
NASA;
OPTICAL INSTRUMENTS;
OXYGEN;
SMOKE;
THERMOCHEMISTRY;
TUNNELS;
VISUALIZATION;
WATER VAPOR;
WIND TUNNELS;
PULSED LASER APPLICATIONS;
|
EID: 57649091235
PISSN: 0277786X
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1117/12.293408 Document Type: Conference Paper |
Times cited : (7)
|
References (9)
|