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Advanced rocket engine nozzles [PDF]
32nd Joint Propulsion Conference and Exhibit, 1996 N. Ponomarev, G. Dumnov, G. Nikulin
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Experimental investigations on pulse detonation rocket engine with various injectors and nozzles
Acta Astronautica, 2011Abstract Pulse detonation engines (PDEs) may represent a revolutionary approach to propulsion. The engine of simple construction can be easily manufactured. The pulse detonation rocket engine (PDRE) used here are 30 mm in inner diameter and 860 mm in length.
Wei Fan +4 more
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Influence of Turbulence Modeling on the Performance Prediction for Rocket Engine Nozzles
Journal of Propulsion and Power, 1999The ow through a nozzle of an advanced rocket engine with and without the injection of a cooling lm has been studied using a Navier–Stokes method. The main focus of this study is the in uence of the choice of the turbulence model on the performance prediction of a lm-cooled nozzle.
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Performance of rocket engine nozzles with slot injection [PDF]
32nd Joint Propulsion Conference and Exhibit, 1996 Dmitry Mel'nikov, Alexy Voinov
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Improvements in rocket engine nozzle and high altitude plume computations
18th Thermophysics Conference, 1983The characteristics of rocket exhaust flow fields are very complex, and many phenomena are involved. Previously, it was necessary to use a multitude of codes to treat a nozzle/plume flow in detail. In connection with both computational and economic standpoints, however, it is desirable to have a single code which can treat all the dominant phenomena in
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Thrust augmentation nozzle (TAN) concept for rocket engine booster applications
Acta Astronautica, 2006Abstract Aerojet used the patented thrust augmented nozzle (TAN) concept to validate a unique means of increasing sea-level thrust in a liquid rocket booster engine. We have used knowledge gained from hypersonic Scramjet research to inject propellants into the supersonic region of the rocket engine nozzle to significantly increase sea-level thrust ...
Mel Bulman, Todd Neill, Scott Forde
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An advanced tubular nozzle extension for liquid rocket engines [PDF]
13th Propulsion Conference, 1977 W. Brunner, W. Buse
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Theoretical liquid rocket engine nozzle flow fields
28th Joint Propulsion Conference and Exhibit, 1992W. J. Phares +2 more
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Investigation of a nozzle tap-off liquid rocket engine scheme [PDF]
32nd Joint Propulsion Conference and Exhibit, 1996 José Nivaldo Hinckel +2 more
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Viscoelastic Properties of Inert Solid Rocket Propellants Exposed to a Shock Wave
Propellants, Explosives, Pyrotechnics, 2022Sarah A Bentil
exaly