2008
DOI: 10.1002/fld.1757
|View full text |Cite
|
Sign up to set email alerts
|

Sliding mesh algorithm for CFD analysis of helicopter rotor–fuselage aerodynamics

Abstract: SUMMARYThe study of rotor-fuselage interactional aerodynamics is central to the design and performance analysis of helicopters. However, regardless of its significance, rotor-fuselage aerodynamics has so far been addressed by very few authors. This is mainly due to the difficulties associated with both experimental and computational techniques when such complex configurations, rich in flow physics, are considered. In view of the above, the objective of this study is to develop computational tools suitable for … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
121
0
5

Year Published

2011
2011
2017
2017

Publication Types

Select...
8
1
1

Relationship

1
9

Authors

Journals

citations
Cited by 206 publications
(130 citation statements)
references
References 18 publications
0
121
0
5
Order By: Relevance
“…For isolated rotors, as well as, rotor/fuselage or rotor/wind-tunnel cases, the rotor and rotor blade motions are then accounted for using mesh velocities. For rotor/fuselage or rotor/wind-tunnel cases, the relative motion of the rotor and the fixed fuselage or tunnel is accounted for the sliding-plane approach [32].…”
Section: Cfd Modelmentioning
confidence: 99%
“…For isolated rotors, as well as, rotor/fuselage or rotor/wind-tunnel cases, the rotor and rotor blade motions are then accounted for using mesh velocities. For rotor/fuselage or rotor/wind-tunnel cases, the relative motion of the rotor and the fixed fuselage or tunnel is accounted for the sliding-plane approach [32].…”
Section: Cfd Modelmentioning
confidence: 99%
“…Rigid or elastic blades can be simulated using static or dynamic computations. HMB2 allows for sliding meshes to simulate rotor-tower interaction cases as described in Steijl and Barakos (2008). Alternatively, overset grids can be used with the details presented in Jarkowski et al (2013).…”
Section: Methodsmentioning
confidence: 99%
“…Rigid or elastic blades can be simulated using static or dynamic computations. HMB3 allows for sliding meshes to simulate rotor-tower interaction cases as described in Steijl and Barakos (2008). Alternatively, overset grids can be used with the details presented in Jarkowski et al (2013).…”
Section: Methodsmentioning
confidence: 99%