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Chaoyang Liu

National University of Defense Technology

Changsha Hunan, 410073

China

SCHOLARLY PAPERS

4

DOWNLOADS

217

TOTAL CITATIONS

2

Scholarly Papers (4)

1.

Study on the Flow Characteristics of Double-Cone in Hypersonic Flows

Number of pages: 30 Posted: 16 Jul 2024
National University of Defense Technology, affiliation not provided to SSRN, National University of Defense Technology, National University of Defense Technology and Central South University
Downloads 110 (669,616)
Citation 2

Abstract:

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Hypersonic flow, High-temperature real gas effects, thermochemical nonequilibrium, Shock wave/boundary layer interaction, Shock/shock interaction

2.

Thermodynamic Performance and Flow Structures Analysis of Supercritical Co2 in a Regenerative Cooling Channel Mounted with Mini-Ribs

Number of pages: 22 Posted: 12 Dec 2023
Central South University, Central South University, Central South University, National University of Defense Technology and Lund University
Downloads 41 (1,209,354)

Abstract:

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regenerative cooling, sCO2, Heat Transfer Enhancement, channel material, Entropy

3.

Flow and Heat Transfer Characteristics of a Regenerative Cooling Channel Using Supercritical Co2 with Different Cross-Section Shapes

Number of pages: 33 Posted: 06 Sep 2024
Central South University, Central South University, Central South University, Central South University, Central South University, National University of Defense Technology and Lund University
Downloads 35 (1,263,436)

Abstract:

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regenerative cooling, supercritical CO2, cross-section shape, flow pattern, channel material

4.

Thermo-Chemical Nonequilibrium Effects on Combustion Characteristics of a Transverse Jet in the Scramjet

Number of pages: 25 Posted: 04 Apr 2024
National University of Defense Technology, National University of Defense Technology, National University of Defense Technology, National University of Defense Technology, National University of Defense Technology, National University of Defense Technology and National University of Defense Technology
Downloads 31 (1,318,317)

Abstract:

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Thermo-chemical nonequilibrium, High Mach number, Supersonic combustion, Two-temperature model, LES