Boeing Rundimentary Landing Gear

back to test case home

Coordinator: FOI
Data Originator:
Data Type: Experimental
Case Status: viewtopicpackage

Page Contents

landing gear2.png

  • allwheelkulites.txt: ASCII file containing experimental unsteady surface pressure probe locations (on wheels)

  • allpostkulites.txt: ASCII file containing experimental unsteady surface pressure probe locations (on posts)


The Boeing Rudimentary Landing Gear (RLG) is a new configuration used in an experimental project funded by Boeing and carried out at NAL (India). The RLG configuration has relatively large axles with square cross-sections and tripping the wheel boundary layers. The trips were designed by CFD in terms of location and size, and found effective. These peculiarities eliminate strong Reynolds number dependence of the previous SLG ("Simplified Landing Gear" by Lazos (2002)) case and enables running the simulations in the fully turbulent mode which, in turn, makes the assessment on the turbulence modelling more “clean” and relevant to the realistic high Reynolds number.

A preliminary description of the RLG configuration is provided here, See the description file for details.

Geometry defined by:

Experimental data:

Guide to Experimental data

Flow Parameters

The freestream velocity is 40 m/s. The Re number based on the wheel diameter (0.406m) and the freestream velocity is 1 million.


Meshes available for this case are listed in the table. Meshes marked with M are mandatory.


Simulation results available for this case are listed below.

Topic attachments
I Attachment Action Size Date Who Comment
pdfpdf ATAAC_ST12_RLG_final_inputs.pdf manage 3234.9 K 2012-04-02 - 12:46 ShiaHuiPeng PDF file of ST12 final inputs
zipzip manage 3841.8 K 2010-02-19 - 14:53 ShiaHuiPeng Geometry files for the Boeing RLG test case (ST12)
docdoc D3-36_ST12_Boeing_RLG_FOI_Shortened_in_D3-36.doc manage 22051.5 K 2012-08-28 - 17:30 ShiaHuiPeng Short version of ST12 (Boeing RLG) to D3-3.6
docdoc D3-36_ST12_Boeing_RLG_FOI_v0.doc manage 72538.0 K 2012-05-25 - 09:37 ShiaHuiPeng Preliminary summary report to D3-36
docdoc D3-36_ST12_Boeing_RLG_FOI_v1.doc manage 60653.5 K 2012-06-26 - 10:43 ShiaHuiPeng ST12 (Boeing RLG) summary (version 1) to D3-36
pdfpdf NAL_Data_File_Definitions_for_ATAAC.pdf manage 1628.5 K 2011-03-31 - 21:07 AlistairRevell  
pdfpdf NAL_Data_File_Definitions_for_ATAAC_revA.pdf manage 1767.8 K 2011-09-12 - 10:48 ShiaHuiPeng Revised file concerning the guidelines of extracting the NAL experimental data.
pdfpdf NAL_Data_File_Definitions_for_ATAAC_revB.pdf manage 1609.2 K 2012-02-10 - 18:03 AlistairRevell  
ziptar RLG_Expt_data_Part1_05July2011.tar manage 81520.0 K 2011-07-06 - 10:00 ShiaHuiPeng Extracted expt. data from ARL experimental dataset - Part 1
pdfpdf RLG_Model_Dimensions.pdf manage 46.8 K 2010-02-19 - 14:59 ShiaHuiPeng RLG model dimensions
elserar RLG_Upload.rar manage 19379.0 K 2011-10-28 - 01:11 SongFu Lastest extraction data in Tecplot style. I am sorry that the notes in the source files are in Chinese.
docdoc ST12_TC_BoeingRLG_Final_version.doc manage 1467.5 K 2012-04-02 - 12:50 ShiaHuiPeng TC description, including required final inputs and format.
docdoc ST12_TC_BoeingRLG_v1b.doc manage 1232.0 K 2010-02-19 - 14:51 ShiaHuiPeng Description file for ST12 (Boeing Rundimentary Landing Gear)
txttxt allpostkulites.txt manage 0.6 K 2010-09-01 - 08:03 CharlesMockett ASCII file containing experimental unsteady surface pressure probe locations (on posts)
txttxt allwheelkulites.txt manage 11.7 K 2010-09-01 - 08:05 CharlesMockett ASCII file containing experimental unsteady surface pressure probe locations (on wheels)
elsebz2 front_000_120.tar.bz2 manage 886304.6 K 2011-03-31 - 18:39 FlavienBillard  
elsebz2 front_120_240.tar.bz2 manage 858229.9 K 2011-03-31 - 18:43 FlavienBillard  
elsebz2 front_240_360.tar.bz2 manage 832274.8 K 2011-03-31 - 18:54 FlavienBillard  
pngpng landing_gear2.png manage 117.7 K 2010-10-07 - 08:34 AlistairRevell  
elsebz2 rear_000_110.tar.bz2 manage 881124.4 K 2011-03-31 - 18:56 FlavienBillard  
elsebz2 rear_110_235.tar.bz2 manage 906367.8 K 2011-03-31 - 18:59 FlavienBillard  
elsebz2 rear_235_360.tar.bz2 manage 853238.2 K 2011-03-31 - 19:06 FlavienBillard  
Edit | Attach | Print version | History: r22 < r21 < r20 < r19 < r18 | Backlinks | Raw View | Raw edit | More topic actions...
Topic revision: r19 - 2012-09-26 - 18:35:53 - FlavienBillard
14 Nov 2019
EU-Flag4ATAAC-website.jpg FP7-coo-RGB.gif

Public Pages:
home Home


Interested in Hybrid RANS-LES Modeling? 5th HRLM Symposium on 19-21 March 2014 See: hrlm_0.png

Related Links:


Advanced Turbulence Simulation for Aerodynamic Application Challenges
A Seventh Framework Project

Copyright © by the contributing authors. Unless noted otherwise, all material on this web site is the property of the contributing authors.