**Jet Aerodynamics and Thrust Calculation****Context:**A medium-sized jet features a fuselage with a diameter of 3.8 meters and a total loaded mass of 85,000 kilograms. Drag on aircraft is predominantly due to the cylindrical shape of the fuselage, with aerodynamic improvements resulting in a drag coefficient of 0.37.**Problem Statement:***Part A* - Calculate the thrust required for the jet's engines to maintain a cruising speed of 230 meters per second at an altitude with an air density of 2.0 kilograms per cubic meter. Provide your answer with appropriate units.**Solution Input:**Use the formula for drag force calculation and express the required thrust as follows:\[ F = \text{Value} \, \text{Units} \]**Calculation Tools:**- Graph and calculator tools are available to assist with solving.- View hints to help understand the approach needed for the formulation.**Educational Objective:**Learn how to compute the thrust necessary for a jet to maintain a specific cruising speed, considering aerodynamic and environmental factors.

Answered: Image /qna-images/answer/51c5965e-aca9-41b6-9469-5f0183d6fc99.jpg

A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jet's engines provide to cruise at 230 m/s at an altitude where the air density is 2.0 kg/m³? Express your answer with the appropriate units. ► View Available Hint(s) F= μA Value Units ?

A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jet's engines provide to cruise at 230 m/s at an altitude where the air density is 2.0 kg/m³? Express your answer with the appropriate units. ► View Available Hint(s) F= μA Value Units ?

College Physics

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ISBN:9781305952300

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter1: Units, Trigonometry. And Vectors

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Question

**Jet Aerodynamics and Thrust Calculation**

**Context:**
A medium-sized jet features a fuselage with a diameter of 3.8 meters and a total loaded mass of 85,000 kilograms. Drag on aircraft is predominantly due to the cylindrical shape of the fuselage, with aerodynamic improvements resulting in a drag coefficient of 0.37.

**Problem Statement:**
*Part A* - Calculate the thrust required for the jet's engines to maintain a cruising speed of 230 meters per second at an altitude with an air density of 2.0 kilograms per cubic meter. Provide your answer with appropriate units.

**Solution Input:**
Use the formula for drag force calculation and express the required thrust as follows:
\[ F = \text{Value} \, \text{Units} \]

**Calculation Tools:**
- Graph and calculator tools are available to assist with solving.
- View hints to help understand the approach needed for the formulation.

**Educational Objective:**
Learn how to compute the thrust necessary for a jet to maintain a specific cruising speed, considering aerodynamic and environmental factors.

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