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Professional Course

Flight Vehicle Aerodynamics

edX, Online
Length
16 weeks
Price
99 USD
Next course start
Inquire for more information See details
Delivery
Virtual Classroom
Length
16 weeks
Price
99 USD
Next course start
Inquire for more information See details
Delivery
Virtual Classroom
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Course description

Flight Vehicle Aerodynamics

This course covers the physics, concepts, theories, and models underlying the discipline of aerodynamics. A general theme is the technique of velocity field representation and modeling via source and vorticity fields, and via their sheet, filament, or point-singularity idealizations.

The intent is to instill an intuitive feel for aerodynamic flowfield behavior, and to provide the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and many other important applications. A few computational methods are covered, primarily to give additional insight into flow behavior, and to identify the primary aerodynamic forces on maneuvering aircraft. A short overview of flight dynamics is also presented.

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Upcoming start dates

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  • Virtual Classroom
  • Online
  • English

Who should attend?

Prerequisites:

Basic mechanics, vector calculus, basic differential equations; good familiarity with basic fluid mechanics concepts (pressure, density, velocity, stress, etc.) similar to the content in 16.101x (however 16.101x is not a requirement).

Course delivery details

This course is offered through Massachusetts Institute of Technology, a partner institute of EdX.

12 hours per week

Costs

  • Verified Track -$99
  • Audit Track - Free

Certification / Credits

What you'll learn

  • To model and predict the aerodynamic flows about wings and bodies
  • To quantify the role of viscous boundary layers in producing drag and limiting lift
  • To quantify and optimize the lift distribution on aircraft wings
  • To reduce and analyze experimental flow survey data to determine profile drag
  • To describe the motion of a maneuvering aircraft and quantify its aerodynamic forces
  • To predict the airloads on unsteady airfoils
  • To estimate the effects of compressibility in high-speed aerodynamic flows

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