Lecture 4 of 24Week 1
Lecture 3B: Lift and Drag for an Infinite Wing... contd.
Prof. Saderla Subrahmanyam · IIT Kanpur
Credits and licence
- From
- UAV Design - Part II, IIT Kanpur (at NPTEL)
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only.
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
- Tweens profiles and older. How courses are placed
All the lectures
- Lecture 01: Introduction to Design Algorithms: Flight Dynamics Point of View
- Lecture 02: Thrust Generation and Power Required
- Lecture 3A: Lift and Drag for Infinite Wing
- Lecture 3B: Lift and Drag for an Infinite Wing... contd.
- Lecture 04: Relation between Aerodynamic center and Center of Pressure
- Lecture 05: Aerodynamic Characteristics of Wing
- Lecture 06: Stability and Criteria for Longitudinal Static Stability
- Lecture 07: Numericals
- Lecture 08: Longitudinal Static Stability- Wing Contribution
- Lecture 09: Flight Demonstration of Flat Plate
- Lecture 10: Numericals Cont.
- Lecture 12: Wing-Tail Contribution and Neutral Point
- Lecture 13: Example problems of wing and tail combination
- Lecture 14: Example problems of wing and tail combination Continued
- Lecture 15: Flight demonstration of identical wing and tail combination
- Lecture 17: Trim Requirements of UAV
- Lecture 18: Example on performance analysis of UAV
- Lecture 19: Weight Estimation and wing Sizing with Example
- Lecture 20: Power Plant Selection with Example
- Lecture 21: Subroutine for takeoff performance (Powerplant selection)
- Lecture 22: Subroutine for Climb Performance (Powerplant Selection)
- Lecture 23: Subroutine for Weight Estimation
- Lecture 24: Subroutine for Planform Geometry Selection
- Lecture 25: Subroutine for Airfoil Selection