default author photo

Zekun Zheng

Tsinghua University

Beijing, 100084

China

SCHOLARLY PAPERS

5

DOWNLOADS

131

TOTAL CITATIONS

0

Scholarly Papers (5)

1.

Critical droplet diameter for flame stabilization in aero-engine shear layers: a reduced energy–mass balance model

Number of pages: 37 Posted: 01 Sep 2025
Civil Aviation University of China, Civil Aviation University of China, Chinese Academy of Sciences (CAS) - Key Laboratory of Light-duty Gas-turbine, Tsinghua University, Beijing Power Machinery Institute and affiliation not provided to SSRN
Downloads 39 (1,209,354)

Abstract:

Loading...

Spray combustion, Droplet evaporation, Aero-engine combustor, Lean blow-out, Critical droplet size

2.

Kinetic Modeling of Surface Deposition for Air-Saturated and Oxygen-Free Aviation Fuels

Number of pages: 34 Posted: 11 Apr 2023
Zekun Zheng, Xinyan Pei, Jiawei Li and Lingyun Hou
Tsinghua University, Tsinghua University, Tsinghua University and Tsinghua University
Downloads 35 (1,249,711)

Abstract:

Loading...

deposition prediction, kinetic model, oxidative deposition, aviation fuel, fuel cooling

3.

A Study of Pyrolysis Reaction Mechanisms for Two Different Sustainable Aviation Fuels Certificated by Civil Aviation Administration of China

Number of pages: 37 Posted: 22 Jul 2025
Civil Aviation University of China, Civil Aviation University of China, affiliation not provided to SSRN, Tianjin University, Beijing Power Machinery Institute, Tsinghua University and affiliation not provided to SSRN
Downloads 28 (1,359,097)

Abstract:

Loading...

Sustainable aviation fuel, Flow reactor, Pyrolysis reaction, Hybrid Chemistry approach (HyChem), NSGA-II

4.

Formation Mechanism of Carbon Deposition on a Venturi Surface in Swirl Combustion Environments

Number of pages: 34 Posted: 25 Aug 2025
Tsinghua University, Tsinghua University, Tsinghua University, Tsinghua University, Tsinghua University and Tsinghua University
Downloads 23 (1,436,435)

Abstract:

Loading...

Carbon deposition, Venturi, Swirl combustion, Coking, Aviation kerosene

5.

Mechanisms of flame stabilization and lean blowout transition governed by turbulent exchange in a swirl-stabilized gas turbine combustor

Number of pages: 57 Posted: 23 Jun 2026
Civil Aviation University of China, Civil Aviation University of China, Civil Aviation University of China, Civil Aviation University of China, affiliation not provided to SSRN, Tsinghua University and Beijing Power Machinery Institute
Downloads 6

Abstract:

Loading...

Swirl-stabilized gas turbine combustor, Lean blowout, Flame stabilization mechanisms, Turbulent exchange, Precessing vortex core