Ramjet Cycles
£3.50
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Ramjet Cycles
£3.50
Topics in this product include the actual Brayton cycle, subsonic combustion ramjet anatomy, the effect of burner temperature and Mach number on performance, engine unstart, and comparing nozzle geometries from conical to aerospike.
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.
PropulsionPage-by-page contents
Propulsion
Page-by-page contents
- 01Ramjet, combustion chamber conditions, flight envelope conditions, burner conditions
- 02Thermodynamic cycle efficiency, actual Brayton T-S diagram
- 03Subsonic combustion, anatomy of subsonic combustion ramjet, ramjet envelope
- 04How to design a ramjet
- 05How to design a ramjet (continued)
- 06Ramjet performance, effect of burner temperature, mach number, and inlet shock strength on performance
- 07Propulsive efficiency, total efficiency, inlet oblique shock compression, optimal inlet cone angle
- 08Engine unstart
- 09Supersonic nozzle design, conical nozzle, bell nozzle
- 10Rao nozzle, plug nozzle, removing bell around plug, aerospike
- 11Comparing nozzle geometries, cone, bell, spike, E-D, scramjet, combustion requirements