Additional Notes Flashcards
(1 cards)
1
Q
Derivation for tail arm length equation.
A
AER324 - Aircraft Dynamics and Control (8 decks)
- Lecture 2 - Overview of Aircraft Static and Dynamic Stability
- Lecture 4 - Aircraft Longitudinal Stability 1
- Lecture 3 - Airplane Stability via Horizontal and Vertical Tail Design
- Lecture 1 - Overview
- Lecture 5 - Aircraft Static Longitudinal Stability 2
- Lecture 9 (after 5) - Static Directional and Lateral Stability. Manoeuvre Stability.
- Tutorial Sheet 1
- Additional Notes
