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 .
Description:
Explore the fundamentals of aircraft performance in this comprehensive 20-hour course. Delve into the history of aviation, starting with George Cayley's concept of lift and drag, and progress to modern airplane components and systems. Learn about aerodynamics, including lift generation, drag polar, and the standard atmosphere. Master the use of measuring instruments like altimeters and airspeed indicators. Analyze static and dynamic performance through equations of motion, thrust and power requirements, and climb performance. Investigate range, endurance, and gliding flight, as well as accelerated flight and V-n diagrams. Study takeoff and landing performance, including the use of high-lift devices. Examine aircraft stability and control, focusing on longitudinal stability, elevator control, and the contributions of wings and tail. Conclude with an introduction to basic aircraft design principles, including wing loading, thrust loading, sweep, and dihedral.