Three-dimensional computations of cross-flow injection and combustion in a supersonic flowA low-storage version of the SPARK3D code which is based on the temporally second-order accurate MacCormack (1969) explicit scheme is used to solve the governing equations for three-dimensional chemically reacting flows with finite-rate chemistry. The code includes a fourth-order compact spatial scheme capable of providing higher order spatial accuracy, and it is used to study two-dimensional linear advection, two-dimensional Euler flow, and three-dimensional viscous flow. Also considered are the injection, mixing, and combustion of hydrogen in a supersonic cross stream.
Document ID
19890054726
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carpenter, M. H. (Analytical Services and Materials, Inc. Hampton, VA, United States)