Detached-Eddy Simulations Over a Simplified Landing Gear

By L. Hedges, A. Travin, P. Spalart. 2002

188 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/a2a90cb1e2e486507a2a8fc18c87c95cf39897b9

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Sanjiva K. Lele
2. Meng Wang
3. Jonathan B. Freund
4. Jochen Fröhlich
5. Dominic von Terzi
6. Tim Colonius
7. Christophe Bogey
8. Christophe Bailly

In Computational Mechanics

1. Sanjiva K. Lele
2. Meng Wang
3. Jonathan B. Freund
4. Jochen Fröhlich
5. Dominic von Terzi
6. Christophe Bogey
7. Christophe Bailly
8. Tim Colonius

In Mechanical Engineering

1. Meng Wang
2. Jochen Fröhlich
3. Dominic von Terzi
4. Sanjiva K. Lele
5. Jonathan B. Freund

Citations in the corpus

• COMPUTATIONAL PREDICTION OF FLOW-GENERATED SOUND (2006, result): “Hedges et al. (2002) computed the noise radiated from an aircraft landing gear model using DES and the FW-H equation and compared results with those from unsteady RANS calculations.”
• Hybrid LES/RANS methods for the simulation of turbulent flows (2008, methodology): “Other applications of this type are the computation of the flow around a simplified landing gear [72,73]”
• Evaluation of linear and nonlinear convection schemes on multidimensional non‐orthogonal grids with applications to KVLCC2 tanker (2009, unknown): “[45].”