36 results on '"Ko, Young‐Sung"'
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2. Testing and Prediction of Heat Exchanger Performance for Liquid Propulsion Engine Based on Simulation Experiment
3. A Study on Ejector Verification Using Natural Intake Method
4. Testing and Prediction of Heat Exchanger Performance for Liquid Propulsion Engine Based on Simulation Experiment
5. Finite element analysis for acoustic characteristics of combustion stabilization devices
6. Heat Transfer Characteristics of the Coil Heat Exchanger Using Helium according to the Shape and Mass Flow Rate Change
7. Metal Oxidation Evaluation Facility in High Temperature/High Pressure/Oxidizer-rich Environment Flow
8. Design and Verification Test of Multiple-Injector Head Arranged in a Row for Combustion Stability Rating Test of a Liquid Rocket Engine
9. A Numerical Analysis on Performance of Parallel Type Ejector for High Altitude Simulation
10. A Numerical Study on Performance Characteristics of STED with various Pressure Ratios and Cone Shapes using Burnt Gas Properties
11. Stability rating tests for the length-optimization of baffles in a liquid propellant combustion chamber using a pulse gun
12. Heat Transfer Characteristics of the Coil Heat Exchanger Using Helium according to the Shape and Mass Flow Rate Change
13. Design and Cold Test of Semi-Freejet High Altitude Environment Simulation Test Facility for High-Speed Vehicle
14. Characteristics of propagating tribrachial flames in counterflow
15. An experiment of the combustion characteristics with laser-induced spark ignition
16. Metal Oxidation Evaluation Facility in High Temperature/High Pressure/Oxidizer-rich Environment Flow
17. Experimental Study on Fluid Viscosity Effects for Centrifugal Turbopump Efficiency
18. Design/Construction/Operation of Experimental Apparatus for Performance Evaluation of Heat Exchanger
19. Numerical Study on Performance Characteristics of Exhaust Gas Properties in Channel and Coil Type Heat Exchanger
20. A Study on Ejector Performance Characteristics by Ejector Geometry/Performance Variables
21. Measurement of Heat Flux in Rocket Combustors Using Plug-Type Heat Flux Gauges
22. Development and Verification Test of a Bi-propellant Thruster Using Hydrogen Peroxide and Kerosene
23. Negative bias illumination stress stability of dual‐active layer amorphous indium‐gallium‐zinc‐oxide thin‐film transistor
24. An Experimental Study on Startup Characteristics of a Center Body Diffuser for High Altitude Simulation
25. An Experimental Study on Performance of Second Throat Exhaust Diffusers of Different Configuration
26. Design and Experimental Verification of Uni-Injector Using Gas Methane and Lox as Propellants
27. Study on Cooling Characteristics of Mixed Gases with Hot Gas of Liquid Rocket Engine and Injected Liquid Nitrogen
28. Estimation of Heat Transfer Coefficient at the Upper Layer of Cryogenic Propellant
29. Design and Cold Flow Test of a Multi-injector Engine using Hydrogen Peroxide/Kerosene
30. Required Pressurant Mass for Cryogenic Propellant Tank with Pressurant Temperature Variation
31. An Experimental Study of a Diffuser Starting Characteristics for Simulating High-Altitude Environment by using a Liquid Rocket
32. Damping Characteristic of Helmholtz Resonator according to Its Geometry and Sound Pressure Level
33. Thick Gate Oxide Integrity Improvement by Sulfuric Peroxide Mixture Cleaning after Thick Gate Oxide Etch
34. Stability Rating Tests of KSR-III Baffled Chamber Using Pulse Gun
35. Characteristics of Dynamic Pressures in Liquid Rocket Thrust Chambers
36. Performance Test of 21AFR Lean Fuel Module at Low and High Operating Conditions
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