16.110 Flight Vehicle Aerodynamics

Class Info

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 available in the Fall semester, and 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.

MIT 16.110 Flight Vehicle Aerodynamics Related Textbooks

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