Performance analysis of an expansion-deflection (E-D) nozzle based on pintle inflection angle von Choi, Junsub, Huh, Hwanil

Volltext

Performance analysis of expansion – deflection nozzles with reduced lengths of nozzle extension at a high-altitude environment von Lee, Joomi, Choi, Junsub, Huh, Hwanil

Volltext

Evaluation of effective emissivity based on manufacturing and mounting scheme for space-borne multilayer insulation von Kim, Jungyeom, Chang, Jin-Soo, Kim, Geon Young, Huh, Hwanil

Volltext

Development of Ultra-Low Specific Speed Centrifugal Pumps Design Method for Small Liquid Rocket Engines von Kim, Hye In, Roh, Tae-Seong, Huh, Hwanil, Lee, Hyoung Jin

Volltext

Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems von Huh, Hwanil, Bang, Hyochoong, Lee, Jaecheong, Lim, Yeerang, Lee, Hosung

Volltext

Drag reduction analysis of counterflow jets in a short penetration mode von Lee, Jaecheong, Lee, Hyoung Jin, Huh, Hwanil

Volltext

Experimental study on flow control system of an electric pump-fed cycle for thrust control von Kim, Geon Young, Lee, Hyoung Jin, Huh, Hwanil

Volltext

Analysis of formation and breakup mechanisms in rotary atomization through spray visualization von Lee, Donghun, You, Gyungwon, Choi, Seongman, Huh, Hwanil

Volltext

Study on the combined effect of various injection conditions on the drag reduction by a counter-flow jet in supersonic flow von Kim, Yongchan, Roh, Tae-Seong, Huh, Hwanil, Lee, Hyoung Jin

Volltext

Numerical study for flame deflector design of a space launch vehicle von Oh, Hwayoung, Lee, Jungil, Um, Hyungsik, Huh, Hwanil

Volltext

Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1: Performance and Operation) von Ha, Donghwi, Roh, Tae-Seong, Huh, Hwanil, Lee, Hyoung Jin

Volltext

Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 2: Core Technologies) von Ha, Donghwi, Roh, Tae-Seong, Huh, Hwanil, Lee, Hyoung Jin

Volltext

Performance Analysis and Mass Estimation of a Small-Sized Liquid Rocket Engine with Electric-Pump Cycle von Lee, Juyeon, Roh, Tae-Seong, Huh, Hwanil, Lee, Hyoung Jin

Volltext

Combustion Efficiencies of Supersonic Flames von Ratner, Albert, Driscoll, James F, Huh, Hwanil, Bryant, Rodney A

Volltext

Numerical Study of Mixing Enhancement by Shock Waves in Model Scramjet Engine von Kim, Ji-Ho, Yoon, Youngbin, Jeung, In-Seuck, Huh, Hwanil, Choi, Jeong-Yeol

Volltext

Study on Numerical Evaluation Method for Cooling Capability of Thermo-Electric Cooler and Effectiveness Assessment of CAE Simulation by using Simplified Thermal Boundary Conditions von Chang, Jin-Soo, Huh, Hwanil

Volltext bestellen

Measured supersonic flame properties - Heat-release patterns, pressure losses, thermal choking limits von Yoon, Youngbin, Donbar, Jeffrey M, Huh, Hwanil, Driscoll, James F

Volltext

Shock-wave-enhancement of the mixing and the stability limits of supersonic hydrogen-air jet flames von Huh, Hwanil, Driscoll, James F.

Volltext

Components Design of an Experimental System for a Lab-Scaled Electric Pump-Fed Cycle von Young Kim, Geon, Jin Lee, Hyoung, Huh, Hwanil

Volltext

Measured lengths of supersonic hydrogen-air jet flames—Compared to subsonic flame lengths—and analysis von Driscoll, James F., Huh, Hwanil, Yoon, Youngbin, Donbar, Jeffrey

Volltext