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Part 1: Document Description
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Citation |
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Title: |
Software Testing: VSPAERO |
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Identification Number: |
doi:10.7910/DVN/0S1R14 |
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Distributor: |
Harvard Dataverse |
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Date of Distribution: |
2021-09-21 |
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Version: |
1 |
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Bibliographic Citation: |
Mariën, Floris, 2021, "Software Testing: VSPAERO", https://doi.org/10.7910/DVN/0S1R14, Harvard Dataverse, V1, UNF:6:hULMSzeOWQZiMFzgiKZxyA== [fileUNF] |
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Citation |
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Title: |
Software Testing: VSPAERO |
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Alternative Title: |
Links to all related documents: |
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Identification Number: |
doi:10.7910/DVN/0S1R14 |
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Authoring Entity: |
Mariën, Floris (Hamburg University of Applied Science) |
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Other identifications and acknowledgements: |
Scholz, Dieter |
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Date of Production: |
2021-07-16 |
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Software used in Production: |
Excel |
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Software used in Production: |
VSPAERO |
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Distributor: |
Harvard Dataverse |
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Access Authority: |
Scholz, Dieter |
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Depositor: |
Scholz, Dieter |
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Date of Deposit: |
2021-07-16 |
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Series Name: |
Digital Library - Projects and Theses - Prof. Dr. Scholz |
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Holdings Information: |
https://doi.org/10.7910/DVN/0S1R14 |
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Study Scope |
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Keywords: |
Engineering, Aviation, Aeronautics, Airplanes, Aerodynamics, Drag (Aerodynamics), Computational fluid dynamics, Flow visualization, Electronic spreadsheets, VLM, drag, induced, Oswald, factor, box wing, aircraft, Luftfahrt, Luftfahrzeug, Flugzeugaerodynamik, Luftwiderstand, Flugzeug, Numerische Strömungssimulation, CFD, Panelverfahren, Tabellenkalkulation, Wirbelgitterverfahren |
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Topic Classification: |
Aerospace |
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Abstract: |
Purpose - Test the aerodynamic analysis code VSPAERO, which is part of OpenVSP from NASA. Apply VSPAERO to calculate the lift curve slope and the span efficiency factor of straight wings (for various aspect and taper ratios) as well as the induced drag of box wings (for various h/b-ratios) relative to their reference wing. --- Methodology - VSPAERO results are compared with results from analytical equations, wind tunnel measurements, and results produced with other aerodynamic codes. --- Findings - VSPAERO offers correct and reliable results, if the simulation is set up with care. The user must always keep an eye on model discretization and refinement, flow conditions, and number of iterations. The Vortex Lattice Method (VLM) and the panel method are best used for different purposes. The VLM shows shorter simulation time and produces reliable results. The panel method is more complicated to use. Numerical results are also good. In addition, the panel method can be used better to visualize flow phenomena. Hoerner's simple approach to induced drag estimation can be used to approximate results of the VLM and the panel method, if a simple correction factor is applied. --- Research Limitations - Most of the tests of VSPAERO have been done with a simple wing geometry, as such much simpler than a full aircraft geometry. --- Practical Implications - VSPAERO can be used with relative ease. It can also be used to show flow phenomena on full aircraft geometry. --- Originality - Repeating simple calculations done many times before does not sound original, but doing this with the relatively new software VSPAERO offering the VLM as well as the panel method seems to be original after all. |
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Kind of Data: |
Program |
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Notes: |
Please use "Tree View" to separate VSP-files from Excel files! |
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Methodology and Processing |
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Sources Statement |
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Data Access |
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Notes: |
This is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, License Version 3. The software is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details: http://www.gnu.org/licenses/gpl.html |
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Other Study Description Materials |
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Related Publications |
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Citation |
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Title: |
Mariën, Floris, 2021. Software Testing: VSPAERO. Master Thesis. Hamburg University of Applied Sciences, Aircraft Design and Systems Group (AERO). Available from: |
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Bibliographic Citation: |
Mariën, Floris, 2021. Software Testing: VSPAERO. Master Thesis. Hamburg University of Applied Sciences, Aircraft Design and Systems Group (AERO). Available from: |
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File Description--f5192335 |
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File: Box_Wing_Calculation.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Calculates induced drag depending on h/b ratio. |
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File Description--f5192337 |
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File: e_theo_f_lambda.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Calculates the theoretical span efficiency factor depending on taper ratio lambda --- Hoerner's function f(lambda) --- and aspect ratio. |
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File Description--f5192341 |
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File: HoernerCurve_PM.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Induced drag is calculated with VSPAERO's Panel Method. It is calculated back to Hoerner's f(lambda) and compared with the function from the "drag bible". |
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File Description--f5192336 |
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File: HoernerCurve_VLM.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Induced drag is calculated with VSPAERO's VLM. It is calculated back to Hoerner's f(lambda) and compared with the function from the "drag bible". |
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File Description--f5192339 |
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File: HoernerCurve_VLMvsPM.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Induced drag is calculated with VSPAERO's VLM and Panel Method. It is calculated back to Hoerner's f(lambda) and compared with the function from the "drag bible". VLM results and PM results are compared |
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File Description--f5192340 |
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File: Lift_Curve_Slope.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Calculates the lift curve slope of different wings and compares this with equations from literature. |
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File Description--f5192338 |
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File: Refinement_Study.tab |
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Notes: |
UNF:6:etnBQL/bDrLvzxarJjVtZg== |
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Looks at how fine the wing needs to be modeled along chord and span to yield good results in VSPAERO's VML and Panel Method. |
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List of Variables: |
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Variable Format: character Notes: UNF:6:i82f3tviQeau2aBFKX/EbQ== |
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f5192341 Location: |
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f5192341 Location: |
Summary Statistics: Min. NaN; StDev NaN; Valid 0.0; Mean NaN; Max. NaN; Variable Format: numeric Notes: UNF:6:g0pwm6JTTr4+4Tl/1Pe9KA== |
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f5192341 Location: |
Summary Statistics: Min. NaN; Max. NaN; StDev NaN; Mean NaN; Valid 0.0; Variable Format: numeric Notes: UNF:6:g0pwm6JTTr4+4Tl/1Pe9KA== |
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f5192341 Location: |
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Variable Format: character Notes: UNF:6:i82f3tviQeau2aBFKX/EbQ== |
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f5192339 Location: |
Summary Statistics: StDev NaN; Valid 0.0; Min. NaN; Max. NaN; Mean NaN; Variable Format: numeric Notes: UNF:6:g0pwm6JTTr4+4Tl/1Pe9KA== |
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f5192339 Location: |
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f5192340 Location: |
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readme.txt |
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text/plain |
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BW005.vsp3 |
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application/octet-stream |
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BW010.vsp3 |
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application/octet-stream |
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BW015.vsp3 |
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application/octet-stream |
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BW020.vsp3 |
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BW025.vsp3 |
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application/octet-stream |
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BW031.vsp3 |
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application/octet-stream |
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BW035.vsp3 |
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BW040.vsp3 |
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BW050.vsp3 |
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BW060.vsp3 |
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BW062.vsp3 |
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BW070.vsp3 |
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application/octet-stream |
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BW080.vsp3 |
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BW093.vsp3 |
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application/octet-stream |
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BW100.vsp3 |
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application/octet-stream |
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RefWing.vsp3 |
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Ais10.vsp3 |
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Ais11.vsp3 |
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application/octet-stream |
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Ais25.vsp3 |
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application/octet-stream |
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application/octet-stream |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
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Tap=1.vsp3 |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
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Notes: |
application/octet-stream |
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Tap=0,3.vsp3 |
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Notes: |
application/octet-stream |
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Tap=0,357.vsp3 |
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Notes: |
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Notes: |
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Label: |
Tap=0,5.vsp3 |
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Notes: |
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Label: |
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Notes: |
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Label: |
Tap=0,8.vsp3 |
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Notes: |
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Label: |
Tap=0.vsp3 |
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Notes: |
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Label: |
Tap=1.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,05.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,1.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,15.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,2.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,3.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,357.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,4.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,5.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,6.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0,8.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=1.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.05.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.1.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.15.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.2.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.3.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.357.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.4.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.5.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.6.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.8.vsp3 |
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Notes: |
application/octet-stream |
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Label: |
Tap=0.vsp3 |
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Notes: |
application/octet-stream |
|
Label: |
Tap=1.vsp3 |
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Notes: |
application/octet-stream |
|
Label: |
RectangularWing.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
SweptTaperedWing.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
SweptWing.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Airbus_A320_Wing_Fuselage_Tail.vsp3 |
|
Notes: |
application/octet-stream |
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Label: |
U12W33_4.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
U16W33_1.vsp3 |
|
Notes: |
application/octet-stream |
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Label: |
U16W33_2.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
U16W33_3.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
U16W33_4.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
U16W33_5.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
U20W33_4.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis12.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis16.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis20.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis24.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis28.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis32.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis4.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis40.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis48.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis60.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis72.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis8.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis84.vsp3 |
|
Notes: |
application/octet-stream |
|
Label: |
Wis33_Uis96.vsp3 |
|
Notes: |
application/octet-stream |