High-order accurate, low numerical diffusion methods for aerodynamics

JA Ekaterinaris - Progress in Aerospace Sciences, 2005 - Elsevier
In recent years numerical methods have been widely used to effectively resolve complex
flow features of aerodynamics flows with meshes that are reasonable for today's computers …

Modern helicopter rotor aerodynamics

AT Conlisk - Progress in aerospace sciences, 2001 - Elsevier
The helicopter rotor wake is among the most complex fluid dynamic structures being three
dimensional and in many cases unsteady. The wake begins at the blade (s) where the flow …

Simulation of rotor in hover: Current state, challenges and standardized evaluation

NS Hariharan, TA Egolf, LN Sankar - 52nd Aerospace Sciences Meeting, 2014 - arc.aiaa.org
A helicopter is subjected to a wide variety of flight conditions with disparate objectives; these
include efficient cruise and hover, and high-performance maneuvering. The hover condition …

Recent improvements to a hybrid method for rotors in forward flight

Z Yang, LN Sankar, MJ Smith, O Bauchau - Journal of Aircraft, 2002 - arc.aiaa.org
THE prediction of rotor blade aerodynamic loads, especially in forward ight, requires
accurate and effi cient modeling of several distinct phenomena. On the advancing side, the …

An overview of wake-breakdown in high-fidelity simulations of rotor in hover

NS Hariharan - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
Wake breakdown is a well-documented computational phenomenon associated with highly
resolved computational hover predictions. As the computational state-of-the-art for hover …

[图书][B] Effective computational methods for wave propagation

NA Kampanis, V Dougalis, JA Ekaterinaris - 2008 - books.google.com
This volume presents several modern, valuable computational methods used to describe
wave propagation phenomena in selected areas of physics and technology. It begins with …

A review of computational techniques for rotor wake modeling

N Hariharan, L Sankar - 38th Aerospace Sciences Meeting and Exhibit, 2000 - arc.aiaa.org
This paper discusses existing techniques for modeling the rotor wake in hover and in
forward flight. It also briefly review extensions of these methods for modeling complete …

EROS—a common European Euler code for the analysis of the helicopter rotor flowfield

P Renzoni, A D'Alascio, N Kroll, D Peshkin… - Progress in Aerospace …, 2000 - Elsevier
The helicopter rotor flowfield is one of the most complex and challenging problems in
theoretical aerodynamics. Its accurate analysis is essential for the design of rotors with …

An efficient and robust method for computing quadrupole noise

KS Brentner, PC Holland - Journal of the American Helicopter …, 1997 - ingentaconnect.com
A new far‐field approximation to the Ffowcs Williams—Hawkings quadrupole source, which
is valid for an in‐plane observer and utilizes preintegration in the direction normal to the …

Investigation of high-order upwinded differencing for vortex convection

BE Wake, D Choi - AIAA journal, 1996 - arc.aiaa.org
WITH the increased performance of workstations and super-computers, three-dimensional
Navier-Stokes solvers are being used by industry today for a myriad of applications. Navier …