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This subject is designed to inform students on the analytical foundations of inviscid subsonic aerodynamics.
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Description
A primary goal of this subject is to equip students with the scientific rigor, applied mathematical complexity, and physical understanding that form the foundation of classical subsonic aerodynamics. Perturbation methods that both simplify mathematical complexity and expand physical understanding of critical phenomenon in fluid flow provides a framework for the subject. The subject offers lectures in classical subsonic aerodynamics at the graduate level on inviscid, subsonic, steady flow over slender aerodynamic bodies. Topics will be selected from: fundamentals of fluid mechanics [review]; singular-perturbation methods [introduction, JIT]; similitude; subsonic flows with axial symmetry; linearized subsonic flow; slender body theory; similarity rules for subsonic flows; two-dimensional flow past a wave-shaped wall; thin wing theory; Kaplan’s higher approximations
Course content
- Singular Perturbation Method Unlimited
- Seminar in Perturbation Methods Unlimited
- Singular Perturbation Methods; Formation of Shock Waves Unlimited
- Fundamental of Fluid Mechanics Unlimited
- Linear Subsonic Flow Unlimited
- Similarity Rules Unlimited
- Bodies of Revolution: Slender Body Theory Unlimited
- Slender Body Theory Unlimited
- Higher Approximations: Slope of the Lift and Moment About Mid-chord Unlimited
- Perturbation Methods / Overview Unlimited
- Thin Wing Theory Unlimited
- Non-linear, Unsteady Transonic Flows Unlimited
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