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This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub/supersonic regimes.
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English
English [CC]
FREE
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Description
16.100 generally has four components: subsonic potential flows, including source/vortex panel methods; viscous flows, including laminar and turbulent boundary layers; aerodynamics of airfoils and wings, including thin airfoil theory, lifting line theory, and panel method/interacting boundary layer methods; and supersonic and hypersonic airfoil theory. Course material varies each year depending upon the focus of the design problem
Course content
- Sensitivity Analysis Unlimited
- Kinematics of a Fluid Element Unlimited
- Stress-Strain Relationship for a Newtonian Fluid Unlimited
- Coordination Transformations for Strain and Stress Rates Unlimited
- Compressible and Incompressible Fluid Element Motion Chart Unlimited
- Compressible Viscous Equations Unlimited
- Compressible Equations Unlimited
- Equations of Aircraft Motion Unlimited
- Brequet Range Equation Unlimited
- Aerodynamic Center Unlimited
- Notes on CQ 1 Unlimited
- Quick Visit to Bernoulli Land Unlimited
- Kutta Condition Unlimited
- Kutta Condition Solution Unlimited
- Thin Airfoil Theory Summary Unlimited
- Important Concepts in Thin Airfoil Theory Unlimited
- Prandtl’s Lifting Line Introduction Unlimited
- Force Calculations for Lifting Line Unlimited
- Trefftz Plane Analysis of Induced Drag Unlimited
- Solution to Problem 1 Unlimited
- Viscous Flow: Stress Strain Relationship Unlimited
- Integral Boundary Layer Equations Unlimited
- Correlation Methods for Integral Boundary Layers Unlimited
- Method of Assumed Profiles Unlimited
- Falkner-Skan Flows Unlimited
- Effect of Turbulent Fluctuations on Mean Flow: Reynolds-Averaging Unlimited
- Poiseuille Flow Through a Duct in 2-D Unlimited
- Duct Flow (cont.) Unlimited
- Laminar Boundary Layer Order of Magnitude Analysis Unlimited
- Solutions of the Laminar Boundary Layer Equations Unlimited
- Similarity in Wind Tunnel Testing Unlimited
- Single Horseshoe Vortex Wing Model Unlimited
- Ground Effect Using Single Vortex Model Unlimited
- Three-Dimensional Wall Effects Unlimited
- Drag Tare Due to Mount Unlimited
- Subsonic Small Disturbance Potential Flow Unlimited
- Critical Mach Number Unlimited
- Behavior of Isentropic Flow in Quasi-1D Unlimited
- Derivation of Sound Wave Properties Unlimited
- Waves in 1D Compressible Flow Unlimited
- Normal Shock Waves Unlimited
- Propagation of Disturbances By a Moving Object Unlimited
- Linearized Compressible Potential Flow Governing Equation Unlimited
- Implications of Linearized Supersonic Flow on Airfoil Lift and Drag Unlimited
- Oblique Shock Waves Unlimited
- Prandtl-Meyer Expansion Waves Unlimited
- Computational Methods for the Euler Equations Unlimited
- Structured vs. Unstructured Grids Unlimited
- Solution Convergence Unlimited
Instructor
Massachusetts Institute of Technology
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