Author: Fenggan ZhuangPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
On the Numerical Simulation of Supersonic Combustion
Author: Fenggan ZhuangNumerical Simulation of Supersonic Combustion
Author: A. NeophytouTowards a Numerical Simulation of Supersonic Mixing & Combustion
Author: Mohammed KamelPublisher: LAP Lambert Academic Publishing
ISBN: 9783659387043
Category :
Languages : en
Pages : 208
Book Description
The design and off-design studies of the hypersonic air-breathing engines face many challenges, due to the complexity of their internal flows. The mixing and combustion processes in Supersonic-Combustion Ramjet (scramjet) engines involve complicated aerothermochemical features, such as: the interactions between shock-waves and boundary-layer, the shock induced-combustion and the recirculation zones. In this study, a numerical solver is developed and validated to be an efficient design tool capable of simulating these complicated flow features of the supersonic combustors. For the code validation, several test cases are considered to monitor the code ability to solve for the diffusive and turbulent fluxes, and the chemical source term. In addition, the code is validated by resolving the transverse sonic injection into supersonic air flow in the case of Helium injection from a flat plate, and in the case of Hydrogen injection in a single-strut scramjet engine. The effectiveness of this injection technique in mixing and flame-holding is demonstrated. The results show good agreement with the previous numerical and experimental investigations, and prove the simulator's accuracy.
A Numerical Simulation of Shock-enhanced Mixing in Supersonic Combustion
Author: Neal David DomelPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 330
Book Description
Numerical Simulation of Supersonic Combustion Problems Using an Implicit LU-SGS Scheme and K-e/q-w Turbulence Closure
Author: P. GerlingerA Two-Dimensional Numerical Simulation of a Supersonic, Chemically Reacting Mixing Layer
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722913984
Category :
Languages : en
Pages : 108
Book Description
Research has been undertaken to achieve an improved understanding of physical phenomena present when a supersonic flow undergoes chemical reaction. A detailed understanding of supersonic reacting flows is necessary to successfully develop advanced propulsion systems now planned for use late in this century and beyond. In order to explore such flows, a study was begun to create appropriate physical models for describing supersonic combustion, and to develop accurate and efficient numerical techniques for solving the governing equations that result from these models. From this work, two computer programs were written to study reacting flows. Both programs were constructed to consider the multicomponent diffusion and convection of important chemical species, the finite rate reaction of these species, and the resulting interaction of the fluid mechanics and the chemistry. The first program employed a finite difference scheme for integrating the governing equations, whereas the second used a hybrid Chebyshev pseudospectral technique for improved accuracy. Drummond, J. Philip Langley Research Center BOUNDARY LAYERS; CHEMICAL REACTIONS; FLUID MECHANICS; MIXING; MIXING LAYERS (FLUIDS); NUMERICAL ANALYSIS; SIMULATION; SUPERSONIC FLOW; CHEBYSHEV APPROXIMATION; COMPUTER PROGRAMS; FINITE DIFFERENCE THEORY; HYPERSONIC AIRCRAFT; SUPERSONIC COMBUSTION RAMJET ENGINES...
3-D Numerical Simulation of Supersonic Reacting Flows in Scramjet Combustor
Author: J. H. LiangA Two-dimensional Numerical Simulation of a Supersonic, Chemically Reacting Mixing Layer
Author: John Philip DrummondPublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 112
Book Description
Numerical Combustion
Author: Alain DervieuxPublisher:
ISBN:
Category : Combustion
Languages : en
Pages : 504
Book Description
Numerical Simulation of Mode Transition in a Hydrogen-fueled Scramjet
Author: Manan Ajay VyasPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
"The Wind-US computational fluid dynamics (CFD) flow solver was used to simulate dual-mode direct-connect ramjet/scramjet engine flowpath tests conducted in the University of Virginia (UVa) Supersonic Combustion Facility (SCF). The objective was to develop a computational capability within Wind-US to aid current hypersonic research and provide insight to flow as well as chemistry details that are not resolved by instruments available."--Leaf iv.