Patent
Rotating combustion chamber for rocket apparatus
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TLDR
In this article, the combustion chamber is rotated during the 'combustion operation' to provide a means for directly increasing the feed of the rocket's engines. But this is not the case in this paper.Abstract:
This invention relates to rocket apparatus adapted for use in aircraft, and relates more particularly to rocket apparatus in which the combustion chamber is rotated during the 'combustion operation. It is one important object of my invention to provide means for directly increasing the feed...read more
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Patent
Rotary reaction motor
TL;DR: In this article, the authors proposed a method for the provision of a jet propelled motor capable of pumping its own propellant, which is called a jet propulsion motor. But this method is not suitable for the use of a combustion chamber provided with an exhaust nozzle.
Patent
Rocket engine nozzle having a notched diverging portion
TL;DR: In a rocket engine nozzle, the diverging portion includes a set of downstream notches running longitudinally from its downstream end and uniformly distributed around the entire periphery of the divergence portion, the total width of all of the notches within any section representing about 1% to 6% of the periphery as mentioned in this paper.