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Continuous Detonation Engine is a new concept of a supersonic combustion engine for aerospace.
The result justifies that continuous detonation engine is a prominent propeller which releases massive impulse.
Coatings of tungsten carbide based hardmetal, nickel based self-fluxing alloy and composites on the basis of NiCrSiB alloy were deposited from these powder by the detonation gun, continuous detonation spraying, and spray fusion process.
A large-scale continuous detonation combustor (CDC) has been designed, fabricated and tested to study the effect of different design elements on the operation process and CDC propulsion performance.
Results indicate continuous detonation propagation through the core of the channel for sufficiently reactive mixtures, while fast-flame propagation occurred for weaker mixtures which do not exhibit detonation initiation at the obstacle face.
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Thus, at predetermined limitations on supply pressures of fuel components and at a fixed mass flow rate of fuel mixture the specific impulse of the LRE prototypes operating in the continuous-detonation mode appeared to be 6 8% higher than the specific impulse of the same LRE prototypes operating in the continuous-combustion mode.
It has been proved experimentally that Zel'dovich thermodynamic cycle with continuous-detonation combustion of hydrogen oxygen mixture in two different LRE prototypes is more energy efficient than the cycle with continuous constant-pressure combustion of the same mixture, other conditions being equal.
The objective of work outlined in this paper was to prove experimentally the energy efficiency of Zel'dovich thermodynamic cycle (cycle with detonative combustion of fuel) by direct comparison of thrust performances of liquid-propellant rocket engine (LRE) prototypes operating in continuous-detonation and continuous-combustion modes using gaseous hydrogen as fuel and gaseous oxygen as oxidizer.
Shallowest ER sinks produce the supercritical transmission mode of the CJ detonation with continuous adaptation of velocity and multicellular structure to local composition.
Detonation of a continuous rod warhead at China Lake, California.
In a supersonic air flow entering the combustor, continuous and longitudinally pulsating modes of hydrogen detonation with the corresponding characteristic frequencies of 1250 and 900 Hz were obtained.
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