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Intakes & Diffusers
£2.50
Topics in this product include isentropic flow relations with and without losses, oblique and bow shocks, supersonic diffuser types, and off-design operation including variable-geometry control inlets.
This is a 8-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.
PropulsionPage-by-page contents
Propulsion
Page-by-page contents
- 01General flight envelope, definitions, hypersonic regime
- 02Deriving isentropic flow relation equations with no losses, stagnation conditions, incompressible flow, defining regimes
- 03Deriving equations with losses, normal shock relations
- 04Oblique shocks, bow shocks, prandtl-meyer function
- 05External diffusers, internal diffusers, supersonic diffusers, normal shock diffusers, converging-diverging diffuser
- 06Example with converging-diverging inlet diffuser
- 07Off-design operation, multiple shock diffusion, spike diffuser, oblique shock diffuser, example
- 08Off design operation, variable geometry control inlet, aircraft vs re-entry vehicles