Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics
<|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 project gives an overview of a selection of geometrical parameters with respect to the tail volume coefficient. A statistic on the basis of 30 aircraft, which differ in their dimensions, was made. One target was to create a graphical method for finding the tail levers arms, both for the horizontal, and the vertical tail. The average tail lever arm for the horizontal tail of all 30 aircraft altogether is 46.2% of their fuselages. The average tail lever arm for the vertical tail of all 30 aircraft altogether is 41.8% of their fuselages. When considering two different configurations, the first configuration (A) is one in which the aircraft have their engines at-tached to the wing and the second configuration (B) is the one in which aircraft have their en-gines attached to the fuselage. The percentages alter to 47% and 44.7% for config' . 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" : ["aircraft","Airplanes--Fuselage","Airplanes--Tail surfaces","Airplanes--Wings","Center of mass","coefficient","Flugzeugentwurf","Hebelarm","Koeffizient","Leitwerk","Levers","Rumpfwerk","Schwerpunkt","Statistics","Statistik","tail","Tragflügel","volume","Volumen","wing"]} <|eot_id|>
 Here is the Description of a dataset. Description:'This project gives an overview of a selection of geometrical parameters with respect to the tail volume coefficient. A statistic on the basis of 30 aircraft, which differ in their dimensions, was made. One target was to create a graphical method for finding the tail levers arms, both for the horizontal, and the vertical tail. The average tail lever arm for the horizontal tail of all 30 aircraft altogether is 46.2% of their fuselages. The average tail lever arm for the vertical tail of all 30 aircraft altogether is 41.8% of their fuselages. When considering two different configurations, the first configuration (A) is one in which the aircraft have their engines at-tached to the wing and the second configuration (B) is the one in which aircraft have their en-gines attached to the fuselage. The percentages alter to 47% and 44.7% for config' . Please return only a json list of at most 3 Keywords corresponding to the Description:.
This project gives an overview of a selection of geometrical parameters with respect to the tail volume coefficient. A statistic on the basis of 30 aircraft, which differ in their dimensions, was made. One target was to create a graphical method for finding the tail levers arms, both for the horizontal, and the vertical tail. The average tail lever arm for the horizontal tail of all 30 aircraft altogether is 46.2% of their fuselages. The average tail lever arm for the vertical tail of all 30 aircraft altogether is 41.8% of their fuselages. When considering two different configurations, the first configuration (A) is one in which the aircraft have their engines at-tached to the wing and the second configuration (B) is the one in which aircraft have their en-gines attached to the fuselage. The percentages alter to 47% and 44.7% for config
aircraft; Airplanes--Fuselage; Airplanes--Tail surfaces; Airplanes--Wings; Center of mass; coefficient; Flugzeugentwurf; Hebelarm; Koeffizient; Leitwerk; Levers; Rumpfwerk; Schwerpunkt; Statistics; Statistik; tail; Tragflügel; volume; Volumen; wing