Boeing Rundimentary Landing Gear

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


Page Contents


landing gear2.png



Description

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.



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

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

Results

Simulation results available for this case are listed below.

Topic attachments
I Attachment Action Size Date Who Comment
zipzip Boeing_RLG_Geometry.zip 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  
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Topic revision: r20 - 2012-11-07 - 16:23:01 - FlavienBillard
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