default author photo

CHEN Qi

Air Force Engineering University

Xi'an

China

SCHOLARLY PAPERS

3

DOWNLOADS

125

TOTAL CITATIONS

0

Scholarly Papers (3)

Research on the Upstream Chamber Pressure and Intake Blockage Characteristics of the Intake-adjustable Rotating Detonation Combustor

Number of pages: 41 Posted: 02 Oct 2025
Air Force Engineering University, 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 42 (1,210,354)

Abstract:

Loading...

Rotating detonation combustor, Variable geometry, Intake adjustable, Intake blockage, Component matching

Research on the Upstream Chamber Pressure and Intake Blockage Characteristics of the Intake-adjustable Rotating Detonation Combustor

Number of pages: 41 Posted: 18 Oct 2025
Air Force Engineering University, 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 10 (1,621,812)

Abstract:

Loading...

Rotating detonation combustor, Variable geometry, Intake adjustable, Intake blockage, Component matching

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:

Loading...

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

3.

Study on the Influence of Cavity Length on the Working Characteristics of the Rotating Detonation Afterburner

Number of pages: 35 Posted: 27 Sep 2025
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 32 (1,318,317)

Abstract:

Loading...

Rotating detonation afterburner, Cavity length, Total pressure recovery coefficient, Combustion efficiency