When dealing with high-pressure releases, be it needed by some operating conditions or
due to an emergency protocol or even to the occurrence of an accident, one has to consider …

An approach for the generation of aerodynamic tables using computational fluid dynamics is
discussed. For aircraft flight dynamics, forces and moments are often tabulated in multi …

The study of rotor–fuselage interactional aerodynamics is central to the design and
performance analysis of helicopters. However, regardless of its significance, rotor–fuselage …

A framework is described and demonstrated for CFD analysis of helicopter rotors in hover
and forward flight. Starting from the Navier–Stokes equations, the paper describes the …

UNLIKE fixed-wing aerodynamic design, which usually in-volves significant computational
fluid dynamics (CFD), rotary-wing design utilizes only a small fraction of the potential that …

THE maneuver capabilities of combat aircraft have highlighted the limitations and
shortcomings of the conventional stability or aerodynamic derivative model for the …

HIGH-SPEED spiked body flows or flows similar to them can appear in a variety of
aerospace applications, such as axisymmetric jet inlets with conical centrebody, 1, 2 ballistic …

EVERY aircraft flying today is required to meet stringent, federally enforced regulations
developed specifically to prevent catastrophic aeroelastic failure. Although, ultimately …

A novel domain element shape parameterization method is presented for computational
fluid dynamics‐based shape optimization. The method is to achieve two aims:(1) provide a …

Dynamic derivatives are used to represent the influence of the aircraft motion rates on the
aerodynamic forces and moments needed for studies of flight dynamics. The use of …