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Aerospace Engineering
Aerodynamics
1. Introduction to Aerodynamics
2. Properties of the Atmosphere
3. Fundamental Principles of Fluid Dynamics
4. Incompressible, Inviscid Flow
5. Incompressible, Viscous Flow
6. Airfoils and Two-Dimensional Wings
7. Three-Dimensional Wings and Finite Wing Theory
8. Compressible Flow Fundamentals
9. Subsonic and Transonic Aerodynamics
10. Supersonic and Hypersonic Aerodynamics
11. Aerodynamic Drag Analysis
12. High-Lift Systems and Flow Control
13. Aircraft Stability and Control
14. Propulsion Integration
15. Experimental Aerodynamics
16. Computational Fluid Dynamics
Subsonic and Transonic Aerodynamics
Compressibility Effects in Subsonic Flow
Prandtl-Glauert Transformation
Compressibility Corrections
Prandtl-Glauert Correction
Karman-Tsien Correction
Limitations and Validity
Critical Mach Number
Determination Methods
Airfoil Shape Effects
Transonic Flow Phenomena
Mixed Subsonic-Supersonic Flow
Local Supersonic Regions
Shock Wave Formation
Weak Shocks
Shock-Boundary Layer Interaction
Transonic Drag Rise
Wave Drag Emergence
Drag Divergence Mach Number
Transonic Aerodynamic Problems
Shock-Induced Separation
Buffet Phenomena
Shock-Stall Interaction
Mach Tuck
Physical Mechanism
Control Implications
The Sound Barrier
Historical Context
Physical Understanding
Overcoming Transonic Difficulties
Transonic Airfoil Design
Supercritical Airfoils
Design Philosophy
Shock Control
Performance Benefits
Shock-Free Design
Adaptive Wing Concepts
Area Rule
Whitcomb's Discovery
Physical Principle
Application to Aircraft Design
Fuselage Shaping
Wing-Body Integration
Supersonic Area Rule
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10. Supersonic and Hypersonic Aerodynamics