Consider a business jet with the following characteristics: • Weight: 25208 kg • Wing area: 53.5 m^2 • Wing span: 21.7 m • Cruise altitude: 10,000 m • Drag polar parameters (cruise): CD0 = 0.015, K= 0.08 • Engine: Number of engines: 2 Max. thrust (at sea level, for 1 engine): 45 kN TSFC (for 1 engine): 0.41 1/h Calculate the velocity for minimum thrust required using the analytical expression (formula)? Calculate the velocity for minimum power required using the analytical expression (formula).? Calculate the maximum velocity using one possible graphical approach, and analytical approach?
Consider a business jet with the following characteristics: • Weight: 25208 kg • Wing area: 53.5 m^2 • Wing span: 21.7 m • Cruise altitude: 10,000 m • Drag polar parameters (cruise): CD0 = 0.015, K= 0.08 • Engine: Number of engines: 2 Max. thrust (at sea level, for 1 engine): 45 kN TSFC (for 1 engine): 0.41 1/h Calculate the velocity for minimum thrust required using the analytical expression (formula)? Calculate the velocity for minimum power required using the analytical expression (formula).? Calculate the maximum velocity using one possible graphical approach, and analytical approach?
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Consider a business jet with the following characteristics:
• Weight: 25208 kg
• Wing area: 53.5 m^2
• Wing span: 21.7 m
• Cruise altitude: 10,000 m
• Drag polar parameters (cruise): CD0 = 0.015, K= 0.08
• Engine: Number of engines: 2
Max. thrust (at sea level, for 1 engine): 45 kN
TSFC (for 1 engine): 0.41 1/h
Calculate the velocity for minimum thrust required using the analytical expression (formula)?
Calculate the velocity for minimum power required using the analytical expression (formula).?
Calculate the maximum velocity using one possible graphical approach, and analytical approach?
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