Summary of Performance Test Plan for a Supercritical CO2 Turbo Alternator Compressor (TAC) with High Backsweep Angle Design > Conferences

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Summary of Performance Test Plan for a Supercritical CO2 Turbo Alternator Compressor (TAC) with High Backsweep Angle Design

Author	조성국, 정용주, 이정익
Conference	2019 한국원자력학회 추계학술발표회
Date	20191024

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이전글Preliminary Study of replacing the constitutive equations in the MARS-KS code to data-based modeling using the Artificial Neural Network
다음글Similitude models for turbine off-design performance prediction under supercritical CO2 condition

Korea Advanced Institute of Science and Technology (KAIST) 291 Daehak-ro Guseong-dong, Yuseong-gu, Daejeon 305-701, Korea / Office: Room 1401, N7-1 (Mechanical Building) TEL : 042 - 350 - 3829 / FAX : 0507 - 083 - 5945 / EMAIL : jeongiklee@kaist.ac.kr Copyright Dept. of Nuclear & Quantum Engineering. All Rights Reserved.

Summary of Performance Test Plan for a Supercritical CO2 Turbo Alternator Compressor (TAC) with High Backsweep Angle Design > Conferences

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Summary of Performance Test Plan for a Supercritical CO2 Turbo Alternator Compressor (TAC) with High Backsweep Angle Design

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