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Standard Atmosphere: Description and Modeling
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Classroom Contents
Introduction to Airplane Performance
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- 1 General Introduction: Airplane Performance Characteristics
- 2 George Cayley: Concept of Lift and Drag
- 3 Introduction to airplane and its components
- 4 Hansa 3 Aircraft and its Primary Systems
- 5 Concept of Lift Aerofoil: Wing : Complete Aircraft
- 6 Drag Polar
- 7 Revision
- 8 Standard Atmosphere: Description and Modeling
- 9 Measuring Instruments: Altimeter, Airspeed Indicator
- 10 Equations of Motion: Static Performance
- 11 Thrust Required, Power Required: Cruise
- 12 Excess Thrust and Power: Climb Angle and Rate of Climb
- 13 Review
- 14 Thrust Required: A Closer Look
- 15 Modeling of CL: Dimensional Analysis
- 16 A Closer Look: Point Mass Model, Dimensional Analysis
- 17 Estimation of Drag Polar Through Flight Test
- 18 Estimation of Rate of Climb
- 19 Revision.
- 20 Range and Endurance
- 21 Range and Endurance: Continued...
- 22 Gliding Flight
- 23 Accelerated Flight
- 24 V-n Diagram
- 25 Revision..
- 26 V stall: Cruise and Manoeuvre
- 27 Flaps:High Lift Devices to Reduce Take off / Landing Distance
- 28 Take off: Warm-up Lecture
- 29 Take off Performance
- 30 Take off Performance:Continued...
- 31 Revision...
- 32 Landing Performance
- 33 Landing Performance: Continued...
- 34 Challanges in Takeoff and Landing: Single and Twin Engines
- 35 Introduction to Static Stability
- 36 Positioning of Center of Pressure for Static Stability
- 37 Revision.....
- 38 Stability and Control: Designers Perspective
- 39 Stability and Control: Designers Perspective Continued...
- 40 Longitudinal Control: Elevator
- 41 Contribution of Wing and Tail: Stability
- 42 Stability: Wing and Tail Contribution
- 43 Control: Elevator
- 44 Control: Delta-e Required
- 45 Control: Delta-e Required continued...
- 46 Design Basics: Wing Loading & Thrust Loading
- 47 Design Basics: Sweep & Dihedral
- 48 Revision .
