Understand and be able to calculate max L/D for an airfoil, suggest a good cruising angle of attack, most efficient operation, etc. Understand the Kutta Condition Able to do all calculations listed in all chapter 4 examples, especially 4.4, 4.5, 4.6… 4.8-4.11 Able to do calculations using Thin Airfoil Theory. Also know material in sections 4.11-13, 4.16 Review for Exam 1 – Chapter 5, Incompressible Flow over Finite Wings Be able to solve all the problems assigned. Understand all wing nomenclature. Be able to understand wing shapes, efficiencies, and best uses. Know material in sections 5.1-
Understand and be able to calculate max L/D for an airfoil, suggest a good cruising angle of attack, most efficient operation, etc. Understand the Kutta Condition Able to do all calculations listed in all chapter 4 examples, especially 4.4, 4.5, 4.6… 4.8-4.11 Able to do calculations using Thin Airfoil Theory. Also know material in sections 4.11-13, 4.16 Review for Exam 1 – Chapter 5, Incompressible Flow over Finite Wings Be able to solve all the problems assigned. Understand all wing nomenclature. Be able to understand wing shapes, efficiencies, and best uses. Know material in sections 5.1-
Aerodynamics%20exam2_review.docx