Aerodynamic Window for Laser Fusion
نویسندگان
چکیده
منابع مشابه
Experimental Study of a Free-vortex Aerodynamic Window
A model of a supersonic free-vortex aerodynamic window has been fabricated and tested. Aerodynamic performance studies show the effectiveness of the model in sealing the simulated laser cavity from higher pressure ambient surroundings. Good starting characteristics and stability of the supersonic window jet are obtained. Static pressure measurements and photographs of the flow fields clearly sh...
متن کاملHigh capacity aerodynamic air bearing (HCAB) for laser scanning applications
A high capacity aerodynamic air bearing (HCAB) has been developed for the laser scanning market. The need for increasing accuracies in the prepress and print plate-making market is causing a shift from ball bearing to air bearing scanners. Aerostatic air bearings are a good option to meet this demand for better performance however, these bearings tend to be expensive and require an additional a...
متن کاملDecision fusion for dual-window- based hyperspectral anomaly detector
In hyperspectral anomaly detection, the dual-window-based detector is a widely used technique that employs two windows to capture nonstationary statistics of anomalies and background. However, its detection performance is usually sensitive to the choice of window sizes and suffers from inappropriate window settings. In this work, a decision-fusion approach is proposed to alleviate such sensitiv...
متن کاملDevelopment of target fabrication for laser-driven inertial confinement fusion at research center of laser fusion
As the basic conditions for laser inertial confinement fusion (ICF) research, the targets are required to be well specified and elaborately fabricated. Because of the characteristics of the targets, the research and fabrication process is a systematically tough task, which needs fundamental and deep insights into film deposition, mechanical machining, precise measurement and assembly, etc. As a...
متن کاملLDV Measurements in the Endwall Region of an Annular Turbine Cascade Through an Aerodynamic Window
Laser-Doppler velocimetry measurements through a one millimeter hole in the casing of an annular turbine cascade were performed in the endwall region downstream of the blade row. Complementary threehole pressure probe measurements were also taken downstream of the nozzle blades, as well as blade surface pressure measurements. The object of this study was to devise methods for the measurement cl...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
سال: 1983
ISSN: 0387-5016,1884-8346
DOI: 10.1299/kikaib.49.548