KOSEN 한인과학기술자네트워크

NAL Newsletter Vol.1 No.1(1998) - Preface to " The NAL Newsletter" - About the New Organization of NAL - NAL Research Activities on Pressure-Sensitive Paint Technology - Construction of a Large High Enthalpy Shock Tunnel HIEST - NAL's Success in Thrust Generation at a Simulated Flight Speed of Mach 8 - Quantitative Measurement of COanda Effect Around a Ball Using PIV - Research on the Causal Factors of Fatal Accidents Involving Cibil Transport Aircraft - Unsteady Flow Analysis of a Turbine Stage - First Annual Review Meeting For NAL-ONERA Research Cooperation Held at ONERA Vol.2 No.1(1999) - Special Issue of NAL's SST project - Development of MuPAL - Pressurizing Fatigue Tests Using A Fuselage Scale Model - A Turbo-Machine for Next Generation Aero-and Space-Planes - Opening a New Avenue in Research Fields of Optical Sensing Techniques and Fullerene Chemistry - Technical Feasibility of SPF Airships for Telecommunications and Earth Observation in the 21st Century Vol.2 No.2(1999) - Special Issue on Space Transportation - The Development of Next Generation Space Transportaiton Systems - The 3rd DLR-NAl Workshop Held at NAL Vol.2 No.3(1999) - Short-Flame, Quick-Quench Burner for Ultra-Low NOx Gas Turbine Combustors - The Production of a High-Efficiency, Three-Steps Thermoelectric Power Generation Element Which Operates at Large Temperature Difference of 800°C Successfully Achieved - Baseline Structural Design of Airframe for Safe Supersonic Flight - GPS Enables Space Transportation Vehicle to Fly Safely - Succeeded in Assembling the Truss by Teleoperation from the Ground - Detecting Unidentified 50 cm-class Diameter Small Objects in 36,000km Geostationary Orbit - Strange Fluid That Goes Down upon Heating Vol.2 No.4(1999) - Special Issue of CFD Vol.3 No.4(2000) - Trial Manufacture of the Tracking Facility for Artificial Satellites - Development of the Onboard Ultrasonic Anemometer and Its Applicatino to the Environmental Observation - Recent Refurbishment of High-Pressure Combustion Facility - Testing a Newly Developed Scramjet Engines with Mach Number 8 - Development of a Common CFD Platform Program "UPACS" - Starting to Use the NAL 60cm Magnetic Suspension and Balance System at a Low SPeed Wind Tunnel - Pressure Sensitive Paint Measurement in Hypersonic Flow 일본 항공우주기술연구소를 안내하는 책자와 Flight Simulator와 극초음속풍동 시스템에 대한 팜플렛이 첨부되어 있다.