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1 |
A Study on Applicability of Turbulence Models for Unsteady Turbulent Flow with Temperature Variation
유근종;전원대;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.1-11,
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2 |
The Effect of Gas Thermochemical Model on the Flowfield of Supersonic Rocket in Propulsive Flight
최환석;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.12-20,
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3 |
Analysis for Combustion Characteristics of Hybrid Rocket Motor
김후중;김용모;윤명원;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.21-29,
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4 |
Bullet Impact Tests for Solid Rocket Motor
윤현걸;최창선;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.30-38,
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5 |
Development of Thrust Measurement System and Study of Calibration in Liquid Rocket Engine
Park, Soo-Hwan;Park, Hee-Ho;Kim, Yoo;Cho, Nam-Choon;Keum, Young-Tag;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.39-46,
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6 |
Effect of droplet length on a burning constant rate of suspended droplet
Han, Jae-Seob;Kim, Seon-Jin;Kim, Yoo;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.47-54,
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7 |
Investigation of Vortical Flow Field Visualization by Micro Water Droplet and Laser Beam Sheet
이기영;손명환;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.55-62,
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8 |
A Fundamental Study of the Supersonic Microjet Flow
정미선;김현섭;김희동;박종호;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.63-70,
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9 |
Computational Analysis of the Flowfield of a Mixer-Ejector Nozzle
Park, Yun-Ho;
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The Korean Society of Propulsion Engineers
, v.6, no.1, pp.71-82,
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