Compressible Flow I
£2.75
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Compressible Flow I
£2.75
Part 1 of 3 in the Compressible Flow series. Topics in this product include isentropic relations, the speed of sound, critical Mach number and drag divergence, normal shock waves, and converging-diverging nozzle and supersonic wind tunnel design.
This is a 9-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
- 01Intro to compressible flow, isentropic relations, 1D compressible flow, continuity
- 02Conservation of momentum, conservation of energy, isentropic relations, compressibility, classification
- 03Subsonic compressible flow, speed of sound, pressure coefficient, propagation of sound waves
- 04Sonic flow, supersonic flow, Mach angle, critical Mach number
- 05Drag divergence Mach number, transonic airfoils, shock waves, normal shock waves
- 06Moving vs stationary normal shocks, quasi 1D compressible flow in a nozzle, varying duct areas
- 07Choking, supersonic nozzle, supersonic diffuser
- 08Con-di nozzle
- 09Continuous supersonic wind tunnel design