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A User’s Guide

Approximate Riemann Solvers

Transverse jet in supersonic crossflows

Topics in Applied Physics is a well-established series of review books, each of which presents a comprehensive survey of a selected topic within the area of applied physics. Edited and written by leading research scientists in the field concerned, each volume contains review contributions covering the various aspects of the topic. Together these provide an overview of the state of the art in the respective field. Topics in Applied Physics is addressed to all scientists at universities and in industry who wish to obtain an overview and to keep abreast of advances in applied physics. The Managing Editors are open to any suggestions for topics coming from the community of applied physicists no matter what the field and encourage prospective book editors to approach them with ideas. 2015 Impact Factor: 0.889

Topics in applied physics

Recent advances in cavity-based scramjet engine- a brief review

Numerical simulation of transverse side jet interaction with supersonic free stream

Thermochemical exploration of hydrogen combustion in generic scramjet combustor

Computational-fluid-dynamics-based design and analysis is presented for a full-scale scramjet combustor with kerosene fuel injected from struts placed in the combustor flowpath. Three-dimensional Navier-Stokes equations are solved with a K-e turbulence model using commercial computational-fluid-dynamics software. Combustion is modeled based on infinitely fast chemical kinetics. Lagrangian dispersed-phase analysis is considered for fueldroplet evaporation and mixing in the supersonic stream. Parametric studies are carried out to investigate the effect of combustor-inlet Mach number and total pressure on the flow development process. A higher combustor-entry Mach number and distributed-fuel-injection system will ensure the existence of predominant supersonic flow in the combustor. Simulations are also carried out to investigate two different kinds of fuel injection struts in the scramjet combustor performance. A distributed-fuel -injection system, required to avoid thermal choking, increases the three-dimensionality of the flowfield.

Debasis Chakraborty

Papers

Numerical simulation of transverse side jet interaction with supersonic free stream

Thermochemical exploration of hydrogen combustion in generic scramjet combustor

Liquid-Fueled Strut-Based Scramjet Combustor Design: A Computational Fluid Dynamics Approach

Optimization of a flight-worthy scramjet combustor through CFD

Numerical exploration of mixing and combustion in ethylene fueled scramjet combustor