• To introduce aerodynamics, ranging from elementary concepts to models of viscous, hypersonic, and rarefied flows by computational fluid dynamics.

  • To define the important aerothermodynamic variables and parameters necessary in atmospheric flight dynamic modeling.

  • To build an appropriate model of aerodynamic force and moment vectors and coefficients for each flow regime.


Shock Wave Mach Number Aerodynamic Force Oblique Shock Normal Shock 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.


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Copyright information

© Birkhäuser Boston 2007

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