NASA NTRS ยท 20140011535
Numerical Analysis of a Rotating Detonation Engine in the Relative Reference Frame
Abstract
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonation engine (RDE) is described. The simulation operates in the detonation frame of reference and utilizes a relatively coarse grid such that only the essential primary flow field structure is captured. This construction yields rapidly converging, steady solutions. Results from the simulation are compared to those from a more complex and refined code, and found to be in reasonable agreement. The performance impacts of several RDE design parameters are then examined. Finally, for a particular RDE configuration, it is found that direct performance comparison can be made with a straight-tube pulse detonation engine (PDE). Results show that they are essentially equivalent.
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Paxson, Daniel E.. 2014-01-13. Numerical Analysis of a Rotating Detonation Engine in the Relative Reference Frame. https://ntrs.nasa.gov/citations/20140011535
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