16.110 Flight Vehicle Aerodynamics
Aerodynamic analysis of flight vehicles using analytical, numerical, and experimental techniques separately and in combination. Matched asymptotic expansions. Farfield behavior. Finite wing theory. Trefftz-plane analysis. Laminar and turbulent boundary layers. Slender body theory. Calculation and measurement of drag components. Aerodynamic stability derivatives.
This class has 16.100 as a prerequisite.
16.110 will not be offered this semester. It will be instructed by M. Drela.
Lecture occurs 1:00 PM to 2:00 PM on Mondays, Wednesdays and Fridays in 33-418.
This class counts for a total of 12 credits.
You can find more information at the http://www.google.com/search?&q=MIT+%2B+16.110&btnG=Google+Search&inurl=https site or on the 16.110 Stellar site.
© Copyright 2015 Yasyf Mohamedali