Ramjet Part 2 – Engine Cycle and Thrust

I have finally figured out that WordPress supports LaTeX, so that makes putting in endless streams of equations much easier! The ideal ramjet engine operates on a Brayton Cycle which is characterised by constant pressure combustion followed by expansion of the combustion products to near ambient pressures. The enthalpy-entropy diagram for this engine cycle is... Continue Reading →

Ramjet Part 1

The basis for all the rocketry and wind tunnel posts discussed  previously are primarily for the development of a micro-ramjet engine. For now I have gone as far as I can on the supersonic wind tunnel and the design has more or less been finalised, all the tunnel wall contours for the test sections are... Continue Reading →

Supersonic Wind Tunnel part 1

Previously I had mentioned the use of water flow to simulate supersonic flow, however after having done some research I've abandoned this approach for now in favour of building a supersonic wind tunnel. The main reason for this is I'd like to some investigation on combustion stability at the small scale I want to operate... Continue Reading →

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