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Yun Wu

Air Force Engineering University

Xi'an

China

SCHOLARLY PAPERS

10

DOWNLOADS

291

TOTAL CITATIONS

2

Scholarly Papers (10)

1.
Downloads 51 (1,063,489)
Citation 2

Tesla Rdc Operation and Performance

Number of pages: 16 Posted: 12 Dec 2024
Air Force Engineering University, Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University and Air Force Engineering University
Downloads 32 (1,341,098)

Abstract:

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RDC, Tesla valve, pressure feedback, mode control, pressure gain

Tesla Rdc Operation and Performance

Number of pages: 16 Posted: 14 Dec 2024
Air Force Engineering University, Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University and Air Force Engineering University
Downloads 19 (1,513,226)
Citation 2

Abstract:

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RDC, Tesla valve, pressure feedback, mode control, pressure gain

2.

Experimental Study on Heat Release Characteristics and Performance Parameters of Two-phase Rotating Detonation Combustor Under Different Equivalence Ratios and Outlet Area Ratios

Number of pages: 34 Posted: 01 Oct 2025
Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University and Air Force Engineering University
Downloads 41 (1,183,237)

Abstract:

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Two-phase RDE, Heat release, Performence, Structural parameters, Incoming-flow parameters

3.

Active Supersonic Cavity Flow Control with a Pulsed-Arc Plasma Actuator Matrix Under Different Phase Modulation Strategies

Number of pages: 39 Posted: 06 May 2025
Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University and affiliation not provided to SSRN
Downloads 39 (1,209,354)

Abstract:

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Supersonic cavity flow, Plasma actuation, flow control, instability

4.

Dynamics of Ozone Generation in Spiral-Tubular Dielectric Barrier Discharge

Number of pages: 25 Posted: 27 Feb 2025
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and Air Force Engineering University
Downloads 39 (1,249,711)

Abstract:

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Spiral-tubular discharge, DBD, Ozone, Reaction pathway analysis, Water

5.

Large Eddy Simulation of Supersonic Cavity Flow Controlled by Pulsed Arc Plasma Actuation

Number of pages: 41 Posted: 05 Jan 2026
Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, affiliation not provided to SSRN and Air Force Engineering University
Downloads 32 (1,318,317)

Abstract:

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Supersonic cavity flow, Plasma actuation, flow control, Shear layer, K-H instability

6.

Research on the Re-wetting Characteristics and Performance Optimization of Coated Pipe during Chill-down Process

Number of pages: 29 Posted: 17 Dec 2025
Air Force Engineering University, Air Force Engineering University, Shanghai Jiao Tong University (SJTU) - Institute of Refrigeration and Cryogenics, affiliation not provided to SSRN, Air Force Engineering University and Air Force Engineering University
Downloads 26 (1,411,822)

Abstract:

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coated pipe, chill-down, temperature gradient, re-wetting, Performance optimization

7.

Operation characteristics of rotating detonation engine with bypass channel

Number of pages: 25 Posted: 03 Sep 2025
Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University, Air Force Engineering University and affiliation not provided to SSRN
Downloads 26 (1,399,036)

Abstract:

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Rotating detonation engine, Bypass channel, Convergent nozzle, Total pressure gain, Combustion efficiency

8.

Aerodynamic Performance of Plasma-Actuated Supersonic Compressor Airfoil at Low Reynolds Number

Number of pages: 102 Posted: 14 Jan 2026
affiliation not provided to SSRN, affiliation not provided to SSRN and Air Force Engineering University
Downloads 13 (1,541,665)

Abstract:

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9.

Stability Analysis of Periodic Orbits in Thermoacoustic Oscillation Using State Sapce Reconstruction with Maximum Predictability

Number of pages: 33 Posted: 18 Apr 2025
affiliation not provided to SSRN, affiliation not provided to SSRN, Xi'an Jiaotong University (XJTU) - School of Mechanical Engineering and Air Force Engineering University
Downloads 12 (1,526,714)

Abstract:

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Thermoacoustic instability, Limit cycle, Floquet exponent

10.

Numerical Study of High-Energy Spark Ignition Characteristics in a Scramjet Combustor

Number of pages: 32 Posted: 01 Jul 2024
affiliation not provided to SSRN, affiliation not provided to SSRN, Air Force Engineering University, Air Force Engineering University, affiliation not provided to SSRN and Air Force Engineering University
Downloads 12 (1,526,714)

Abstract:

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Ignition, Scramjet Engine, Supersonic combustion, High-energy spark