Reverse Engineering of Passenger Jets – Classified Design Parameters
<|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:'This thesis explains how the classified design parameters of existing passenger jets can be determined. The classified design parameters are; the maximum lift coefficient for landing and take-off, the maximum aerodynamic efficiency and the specific fuel consumption. The entire concept is based on the preliminary sizing of jet powered civil aeroplanes. This preliminary sizing is explained in detail because it is the foundation of the final result. The preliminary sizing is combined using reverse engineering which is not a strict method. Therefore, only the basics are explained. By applying reverse engineering on the preliminary sizing and aiming for the classified design parameters as output, formulas are derived to calculate the maximum lift coefficients, the maximum aerodynamic efficiency and the specific fuel consumption. The goal is t' . 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","Aerodynamik","Aeronautics","Aeroplanes","Airplanes","Airplanes--Fuel consumption","Airplanes—Landing","Airplanes—Takeoff","Auftriebsbeiwert","Computer software","Cruise","Design","Dimensionierung","Electronic spreadsheets","Entwurf","Flugzeug","Gleitzahl","Glide ratio","Kraftstoffverbrauch","Landung","L/D","Lift (Aerodynamics)","Luftfahrt","Luftfahrttechnik","Luftfahrzeug","Passagier","Passagierflugzeug","Preliminary sizing","Reiseflug","Reverse engineering","Reverse Engineering","Start","Verification (Logic)","Verifikation"]} <|eot_id|>
 Here is the Description of a dataset. Description:'This thesis explains how the classified design parameters of existing passenger jets can be determined. The classified design parameters are; the maximum lift coefficient for landing and take-off, the maximum aerodynamic efficiency and the specific fuel consumption. The entire concept is based on the preliminary sizing of jet powered civil aeroplanes. This preliminary sizing is explained in detail because it is the foundation of the final result. The preliminary sizing is combined using reverse engineering which is not a strict method. Therefore, only the basics are explained. By applying reverse engineering on the preliminary sizing and aiming for the classified design parameters as output, formulas are derived to calculate the maximum lift coefficients, the maximum aerodynamic efficiency and the specific fuel consumption. The goal is t' . Please return only a json list of at most 3 Keywords corresponding to the Description:.
This thesis explains how the classified design parameters of existing passenger jets can be determined. The classified design parameters are; the maximum lift coefficient for landing and take-off, the maximum aerodynamic efficiency and the specific fuel consumption. The entire concept is based on the preliminary sizing of jet powered civil aeroplanes. This preliminary sizing is explained in detail because it is the foundation of the final result. The preliminary sizing is combined using reverse engineering which is not a strict method. Therefore, only the basics are explained. By applying reverse engineering on the preliminary sizing and aiming for the classified design parameters as output, formulas are derived to calculate the maximum lift coefficients, the maximum aerodynamic efficiency and the specific fuel consumption. The goal is t
Aerodynamics; Aerodynamik; Aeronautics; Aeroplanes; Airplanes; Airplanes--Fuel consumption; Airplanes—Landing; Airplanes—Takeoff; Auftriebsbeiwert; Computer software; Cruise; Design; Dimensionierung; Electronic spreadsheets; Entwurf; Flugzeug; Gleitzahl; Glide ratio; Kraftstoffverbrauch; Landung; L/D; Lift (Aerodynamics); Luftfahrt; Luftfahrttechnik; Luftfahrzeug; Passagier; Passagierflugzeug; Preliminary sizing; Reiseflug; Reverse engineering; Reverse Engineering; Start; Verification (Logic); Verifikation