Aerodynamics Lecture Notes
This note covers the following topics: Kinematics of a Fluid Element, Stress-Strain Relationship for a Newtonian Fluid, Brequet Range Equation, Coordination Transformations for Strain and Stress Rates, Equations of Aircraft Motion, Viscous Flow, Integral Boundary Layer Equations, Correlation Methods for Integral Boundary Layers, Falkner-Skan Flows, Three-Dimensional Wall Effects, Subsonic Small Disturbance Potential Flow, Waves in 1D Compressible Flow, Normal Shock Waves, Linearized Compressible Potential Flow Governing Equation, Oblique Shock Waves, Prandtl-Meyer Expansion Waves, Computational Methods for the Euler Equations, Solution Convergence.
Author(s): Prof. David Darmofal
NA Pages 
Introduction to Aerodynamics for Flight
This note covers What do we want from aerodynamics, Basic ideas from 2D, Differences between 2D and 3D and the importance of unsteadiness.
Author(s): Brown University
51 Pages
Aerodynamics by Dr. Krishna Anand V
This note introduces the concepts of mass,momentum and energy conservation relating to aerodynamics.Also it make the student understand the concept of vorticity, irrotationality,theory of airfoils and wing sections.
Author(s): Dr. Krishna Anand V
106 Pages
This note covers the following topics: Kinematics of a Fluid Element, Stress-Strain Relationship for a Newtonian Fluid, Brequet Range Equation, Coordination Transformations for Strain and Stress Rates, Equations of Aircraft Motion, Viscous Flow, Integral Boundary Layer Equations, Correlation Methods for Integral Boundary Layers, Falkner-Skan Flows, Three-Dimensional Wall Effects, Subsonic Small Disturbance Potential Flow, Waves in 1D Compressible Flow, Normal Shock Waves, Linearized Compressible Potential Flow Governing Equation, Oblique Shock Waves, Prandtl-Meyer Expansion Waves, Computational Methods for the Euler Equations, Solution Convergence.
Author(s): Prof. David Darmofal
NA Pages
This note covers the following topics: Historical Background, Parts of an Aircraft, Stability, Aerospace Terminology, Forces on Aircraft, Lift and Drag, Airfoils, Pi Theorem, Energy Equation, Substantial Derivative, Pathline and stream line, Uniform Flow, source flow, Uniform Flow, Propulsion, Operational Envelopes, Standard Atmosphere, Air-breathing Engines, Aircraft Performance, Rocket Engines, Review of Gas Dynamics, H-K Diagram, Normal shock wave, Flow with heat addition, Flow with friction.
Author(s): Ehsan Roohi Golkhatmi
NA Pages
