This presentation describes experimental and computational approaches to measuring pressure gain in the various devices currently under investigation wherein the working fluid undergoes a pressure gain combustion (PGC) process. Pressure gain is essentially a measure of the fluid availability for work or thrust production. The devices covered are Resonant Pulse Combustors, Internal Combustion Wave Rotors, Pulse Detonation Engines, and Rotating Detonation Engines. The approaches to pressure gain measurement differ in each device. However, all of the approaches attempt to address the fundamental challenges of PGC system measurement: the extremely harsh environment which makes instrumentation difficult, and the temporal and spatial non-uniformi...
This paper describes a new method for calculating the performance of pressure gain combustors for ga...
Pulse-combustor configurations developed in recent studies have demonstrated performance levels at h...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
Over the past few decades, there has been significant research into propulsion concepts attempting t...
A particular type of pressure gain combustion (PGC) device is described, which is under investigatio...
Pressure Gain Combustion (PGC) is under investigation as a means to improve the thermal efficiency o...
Pressure gain combustion has been known to be more thermodynamically efficient than its constant pre...
Various aspects of the pressure-gain combustion engine are investigated analytically and experimenta...
NASA has undertaken a systematic exploration of many different facets of pressure gain combustion ov...
Pulse-combustor configurations developed in recent studies have demonstrated performance levels at h...
Combustion and evaporation processes occurring in a closed chamber can result in significant pressur...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
This paper describes a new method for calculating the performance of pressure gain combustors for ga...
Conventional gas turbines are approaching their efficiency limits and performance gains are becoming...
This paper describes a new method for calculating the performance of pressure gain combustors for ga...
Pulse-combustor configurations developed in recent studies have demonstrated performance levels at h...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
Over the past few decades, there has been significant research into propulsion concepts attempting t...
A particular type of pressure gain combustion (PGC) device is described, which is under investigatio...
Pressure Gain Combustion (PGC) is under investigation as a means to improve the thermal efficiency o...
Pressure gain combustion has been known to be more thermodynamically efficient than its constant pre...
Various aspects of the pressure-gain combustion engine are investigated analytically and experimenta...
NASA has undertaken a systematic exploration of many different facets of pressure gain combustion ov...
Pulse-combustor configurations developed in recent studies have demonstrated performance levels at h...
Combustion and evaporation processes occurring in a closed chamber can result in significant pressur...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
This paper describes a new method for calculating the performance of pressure gain combustors for ga...
Conventional gas turbines are approaching their efficiency limits and performance gains are becoming...
This paper describes a new method for calculating the performance of pressure gain combustors for ga...
Pulse-combustor configurations developed in recent studies have demonstrated performance levels at h...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...