Compressible Flow III
£3.50
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Compressible Flow III
£3.50
Part 3 of 3 in the Compressible Flow series. Topics in this product include unsteady compressible waves and the method of characteristics, acoustic theory, wave reflection, regions of influence and dependence, and 2D supersonic flow through to supersonic nozzle design.
This is a 11-page PDF scan of handwritten notes, featuring clickable PDF bookmarks so you can jump straight to any page in a PDF viewer such as Adobe Acrobat. Complete page-by-page contents can be found below so you know exactly what's inside before you buy.
AerodynamicsPage-by-page contents
Aerodynamics
Page-by-page contents
- 01Unsteady 1D compressible flow, unsteady shocks, example, stagnation quantities, reflecting unsteady shocks
- 02Example, unsteady waves, visualising acoustic theory
- 03Acoustic theory derivation, LR and RR solutions
- 04Finite strength isentropic waves
- 05Method of characteristics, conservation of mass, conservation of momentum
- 06Wave reflection, approximating non-simple regions, example
- 07Example continued, regions of influence and dependence
- 08Steady 2D supersonic flow: method of characteristics, Prandtl-Meyer expansions
- 09Boundary conditions, sonic line, transonic airfoil
- 10Supersonic jets, supercritical airfoil
- 11Supersonic nozzle design