This book is elegantly composed for an average student who is interested in learning the
fundamentals of aerodynamics. Even if they do not have any background in aerodynamics …

This paper describes a numerical investigation on the effects of wall temperature and
leading-edge bluntness on hypersonic laminar separation induced by a finite-span …

THE Fundamental Aero Program (FAP) within NASA has a goal of reducing uncertainties in
hypersonicflow simulation by 50%. The target goal started as a subjective assessment of the …

Because of viscous interaction in hypersonic flows, the state of the boundary layer
significantly influences possible shock-wave boundary-layer interaction as well as surface …

A numerical study was undertaken using the commercial computational-fluid-dynamics code
CFD++ to analyze the combustion behavior of a three-dimensional nonuniform-compression …

In hypersonic flows, the numerical solution is strongly influenced by the local grid resolution.
The mesh-adaptive simulations within this paper are a good approach to achieve solutions …

A combined experimental as well as computational analysis of a complete scramjet
demonstrator model has been initiated. The experimental tests will take place under real …

One of the major challenges to scramjet propulsion is the ability to operate over a wide
range of Mach numbers. The dual-mode scramjet has the advantage that it can operate …

This paper shall present the numerical results of an investigation into the effect of wall to
freestream temperature on boundary layer separation for a nominal flat plate/15degree …

Scramjets are hypersonic airbreathing engines that utilize the unique technology of
supersonic combustion. Besides supersonic combustor and nozzle, the intake and …