UNIVERSITY OF TORONTO
FACULTY OF APPLIED SCIENCE AND ENGINEERING
AER302H1S: AIRCRAFT FLIGHT
Mid-Term Test, March 2 2009
Instructor: Prof. P. R. Grant
This is Type X test.
Only non-programmable electronic calculators are allowed.
Total marks: 100
65.35 3.5 2 baa Humans n8: Seaman uEEoou 2F.
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an. 8 3:03.535 45650.8 a: 3:055? :82 H JD
E05508 t: ES H 40
Esau 1.62 H u
swam mam? H a when?
a a u
22.8 ha 8 G a u N
Chapter 2 (Sherman Notes) Updated 9/16/15
1. Pitch Static Stability
The most common models for the lift and drag forces on an airfoil are:
C L C L0 C L
CD CDmin K CL2 .
The key variable in (1) is the angle of attack, . Let x cg denote the distanc