Software Testing: VSPAERO
<|begin_of_text|><|start_header_id|>system<|end_header_id|> You are a research archivist expert in dataset metadata. Answer the question truthfully.  <|eot_id|><|start_header_id|>user<|end_header_id|> Here is the Description of a dataset. Description:'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 si' . Please return only a json list of at most 3 Keywords corresponding to the Description:.<|eot_id|><|start_header_id|>assistant<|end_header_id|> {"Answer" : ["Aerodynamics","Aeronautics","aircraft","Airplanes","Aviation","box wing","CFD","Computational fluid dynamics","drag","Drag (Aerodynamics)","Electronic spreadsheets","factor","Flow visualization","Flugzeug","Flugzeugaerodynamik","induced","Luftfahrt","Luftfahrzeug","Luftwiderstand","Numerische Strömungssimulation","Oswald","Panelverfahren","Tabellenkalkulation","VLM","Wirbelgitterverfahren"]} <|eot_id|>
 Here is the Description of a dataset. Description:'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 si' . Please return only a json list of at most 3 Keywords corresponding to the Description:.
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 si
Aerodynamics; Aeronautics; aircraft; Airplanes; Aviation; box wing; CFD; Computational fluid dynamics; drag; Drag (Aerodynamics); Electronic spreadsheets; factor; Flow visualization; Flugzeug; Flugzeugaerodynamik; induced; Luftfahrt; Luftfahrzeug; Luftwiderstand; Numerische Strömungssimulation; Oswald; Panelverfahren; Tabellenkalkulation; VLM; Wirbelgitterverfahren