The aerodynamic design of multi-element high-lift systems for transport airplanes

CP Van Dam - Progress in Aerospace Sciences, 2002 - Elsevier
High-lift systems have a major influence on the sizing, economics, and safety of most
transport airplane configurations. The combination of complexity in flow physics, geometry …

Prediction of high lift: review of present CFD capability

CL Rumsey, SX Ying - Progress in Aerospace Sciences, 2002 - Elsevier
A survey is conducted of CFD methods applied to the computation of high-lift multi-element
configurations over the last 10–15 years. Both 2-D and 3-D configurations are covered. The …

Sensitivity analysis of geometric parameters on the aerodynamic performance of a multi-element airfoil

MAS PM, LP Raj - Aerospace Science and Technology, 2023 - Elsevier
High-lift devices play a vital role in most commercial airplanes' design, maintenance, safety,
and performance. The design of high-lift devices is complex due to the flow physics …

Unstructured viscous grid generation by the advancing-layers method

S Pirzadeh - AIAA journal, 1994 - arc.aiaa.org
DURING the past few years, computational fluid dynamics has progressed to the point that
routine, accurate inviscidflow computations are now possible for practical, realistic …

Grid quality and resolution issues from the drag prediction workshop series

DJ Mavriplis, JC Vassberg, EN Tinoco, M Mani… - Journal of …, 2009 - arc.aiaa.org
The drag prediction workshop series, held over the last six years and sponsored by the AIAA
Applied Aerodynamics Committee, has been extremely useful in providing an assessment of …

Recent turbulence model advances applied to multielement airfoil computations

CL Rumsey, TB Gatski - Journal of aircraft, 2001 - arc.aiaa.org
A one-equation linear turbulence model and a two-equation nonlinear explicit algebraic
stress model (EASM) are applied to the ow over a multielement airfoil. The effect of the K–" …

An active flow circulation controlled flap concept for general aviation aircraft applications

G Jones, S Viken, A Washburn, L Jenkins… - 1st Flow control …, 2002 - arc.aiaa.org
A recent focus on revolutionary aerodynamic concepts has highlighted the technology
needs of general aviation and personal aircraft. New and stringent restrictions on these …

Unstructured-mesh discretizations and solvers for computational aerodynamics

DJ Mavriplis - AIAA journal, 2008 - arc.aiaa.org
An overview of current unstructured-mesh discretization and solution techniques is given.
Cell-centered vs vertexcentered discretizations are discussed, as well as issues of grid …

Reconstruction of turbulent fluctuations using a hybrid RANS/LES approach

E Labourasse, P Sagaut - Journal of Computational Physics, 2002 - Elsevier
A hybrid RANS/LES approach is presented and assessed considering several flows, which
can be interpreted as the most general case of the NLDE approach as defined by Morris et …

[图书][B] An unstructured grid generation and adaptive solution technique for high Reynolds number compressible flows

GA Ashford - 1996 - search.proquest.com
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about
complex geometries is described. The solution methodology consists of three main …