Pulse detonation propulsion: challenges, current status, and future perspective

GD Roy, SM Frolov, AA Borisov, DW Netzer - Progress in Energy and …, 2004 - Elsevier
The paper is focused on recent accomplishments in basic and applied research on pulse
detonation engines (PDE) and various PDE design concepts. Current understanding of gas …

Propulsive performance of airbreathing pulse detonation engines

F Ma, JY Choi, V Yang - Journal of propulsion and power, 2006 - arc.aiaa.org
PULSE detonation engines (PDEs) are unsteady propulsion devices that produce thrust by
using repetitive propagating detonation. Extensive efforts have been applied to circumvent …

Thrust chamber dynamics and propulsive performance of single-tube pulse detonation engines

F Ma, JY Choi, V Yang - Journal of propulsion and power, 2005 - arc.aiaa.org
Thrust Chamber Dynamics and Propulsive Performance of Single-Tube Pulse Detonation
Engines Page 1 JOURNAL OF PROPULSION AND POWER Vol. 21, No. 3, May–June 2005 …

Experimental investigation of rotating detonation rocket engines for space propulsion

RD Smith, SB Stanley - Journal of Propulsion and Power, 2021 - arc.aiaa.org
The performance (specific impulse, I sp) of a modular, 150-lb f-class rotating detonation
rocket engine (RDRE) was measured with three gaseous fuels (methane, ethane, and …

Two-dimensional temperature in a detonation channel using two-color OH planar laser-induced fluorescence thermometry

SW Grib, CA Fugger, PS Hsu, N Jiang, S Roy… - Combustion and …, 2021 - Elsevier
This work demonstrates single-shot, two-dimensional temperature measurements in a
premixed linear detonation channel using two-color OH planar laser-induced fluorescence …

Model for the performance of airbreathing pulse-detonation engines

E Wintenberger, JE Shepherd - Journal of propulsion and power, 2006 - arc.aiaa.org
PULSE-DETONATION engines (PDEs) are propulsion systems based on the intermittent use
of detonative combustion. A typical airbreathing PDE consists of an inlet, a series of valves …

Performance modeling of pulse detonation engines using the method of characteristics

JT Peace, FK Lu - Aerospace Science and Technology, 2019 - Elsevier
A quasi-one-dimensional method of characteristics (MOC) model is developed to evaluate
the single-cycle gasdynamic flow field and associated propulsive performance of a fully-and …

Parametric investigation of thrust augmentation by ejectors on a pulsed detonation tube

J Wilson, A Sgondea, DE Paxson… - Journal of Propulsion and …, 2007 - arc.aiaa.org
THE pulsed detonation engine was studied by Nicholls et al.[1] as a thrust-producing device
as early as 1957. Interest then seems to have lapsed until it was revived in 1991 by …

Multiple-point ignition as a driver of flame acceleration at the early stage of burning in channels

C Miao, DM Valiev - Combustion and Flame, 2024 - Elsevier
In the present study, flame acceleration driven by an array of multiple ignition kernels,
equally spaced in the axial direction of a channel closed at one end, is studied numerically …

Performance measurements of multicycle pulse-detonation-engine exhaust nozzles

D Allgood, E Gutmark, J Hoke, R Bradley… - Journal of Propulsion …, 2006 - arc.aiaa.org
PULSE detonation engines (PDE) use controlled periodic deto-nations of a combustible
mixture to generate thrust. 1 Detonation combustion differs from the more commonly used …