Aerodynamics II
OVERVIEW
CEA CAPA Partner Institution: Universidad Carlos III de Madrid
Location: Madrid, Spain
Primary Subject Area: Aerospace Engineering
Instruction in: English
Course Code: 14173
Transcript Source: Partner Institution
Course Details: Level 400
Recommended Semester Credits: 3
Contact Hours: 42
Prerequisites: Advanced Mathematics, Fluid Mechanics I and II, Aerodynamics I
DESCRIPTION
Incompressible 3D potential flow. Basic solutions. Green's formula
Wings of finite span in incompressible flows. Lifting surface theory. Application to Slender wings. Numerical lifting surface method.
Wings of finite span in supersonic flows. Linearized protential. Supersonic source. Subsonic and supersonic edges. Evvard formulas and integration rules. Global characteristics of supersonic wings.
Wings of finite span in subsonic flows. Prandtl Glauert analogy. Swept wings.
Slender body theory. Problem formulation for revolution bodies. Transversal forces. Longitudinal forces.
Experimental aerodynamics. Similarity principles. Wind tunnel design. Measurement and visualisation techniques
Wings of finite span in incompressible flows. Lifting surface theory. Application to Slender wings. Numerical lifting surface method.
Wings of finite span in supersonic flows. Linearized protential. Supersonic source. Subsonic and supersonic edges. Evvard formulas and integration rules. Global characteristics of supersonic wings.
Wings of finite span in subsonic flows. Prandtl Glauert analogy. Swept wings.
Slender body theory. Problem formulation for revolution bodies. Transversal forces. Longitudinal forces.
Experimental aerodynamics. Similarity principles. Wind tunnel design. Measurement and visualisation techniques
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