Lecture 7-Aircraft Performance 1

Lecture 7-Aircraft Performance 1 - AOE 2104-Aerospace and...

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Click to edit Master subtitle style AOE 2104--Aerospace and Ocean Engineering Fall 2010 Virginia Tech 30 Sept 2010 Lecture 7 AOE 2104 Introduction to Aerospace Engineering Lecture 7 Aircraft Flight Mechanics Performance
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Click to edit Master subtitle style Virginia Tech 1. As you slow down below the minimum drag speed, why do you need to add more thrust to maintain level flight? 2. What is the coefficient of pressure? 3. How does thrust required vary with altitude? 4. What dictates the minimum and maximum velocity you can fly at at a given altitude? 5. How does thrust available vary with velocity for a turbojet? 6. How does power available vary with velocity for a propeller? 7. What is power? 8. How do you compute the rate of climb? 9. How does thrust available vary with altitude? AOE 2104--Aerospace and Ocean Engineering Fall 2010 30 Sept 2010 Lecture 7
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Click to edit Master subtitle style Virginia Tech V P R Aircraft Performance – SSSL Power Required distance distance time energy force Power force time ti P V me T × = × = = = Power Available = Thrust x Velocity Power Required = Drag x Velocity AOE 2104--Aerospace and Ocean Engineering Fall 2010 30 Sept 2010 Lecture 7
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Click to edit Master subtitle style Virginia Tech Derivations!!! AOE 2104--Aerospace and Ocean Engineering Fall 2010 30 Sept 2010 Lecture 7
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Click to edit Master subtitle style Virginia Tech Aircraft Performance – Power Required Variation with Altitude PR V Move to the  right and up  with altitude AOE 2104--Aerospace and Ocean Engineering Fall 2010 30 Sept 2010 Lecture 7
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Virginia Tech Aircraft Performance – Power Available Curve P V Move to the  right and up 
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This note was uploaded on 10/02/2011 for the course AERO 1234 at Virginia Tech.

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Lecture 7-Aircraft Performance 1 - AOE 2104-Aerospace and...

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