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The structure, properties, preparation methods, and characterization techniques of BP. As a typical 2D layered material, black phosphorus (BP) demonstrates exceptional promise in various fields, particularly in energy storage for alkali metal‐ion batteries. However, its distinctive structure and properties, together with the compositional complexity of
Yunqing Wang +7 more
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Pressure Effect on the Rheological Behavior of Highly Filled Solid Propellant During Extrusion Flow. [PDF]
Zhang J +5 more
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Experimental and machine learning-driven assessment of IS 2062 steel under double-base propellant combustion conditions. [PDF]
Singh H +3 more
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Real time 3D monitoring of sintering ore temperature enabled by temporal fusion transformers. [PDF]
Jiang Y +10 more
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Numerical Study on Unstable Combustion: Combustion Instability and Combustion Noise
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On nonlinear combustion instability
33rd Joint Propulsion Conference and Exhibit, 1997A crucial need in rocket motor development programs is a valid analytical/computational model of nonlinear combustion instability. The motor designer frequently must attempt to estimate not only the probability that a particular acoustic mode may "tend to grow," but what will be the amplitude of the oscillations if they are triggered in some way.
S. Malhotra +3 more
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Mechanisms of combustion instability
Symposium (International) on Combustion, 1965This paper presents results of a study aimed at understanding mechanisms involved in triggering, amplification, and suppression of acoustic waves, due to presence of flames. Experiments performed demonstrate that strong interactions between acoustic and flame oscillations can exist through flow oscillations, and that these interactions are due to ...
Tau-Yi Toong +3 more
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On the Hybrid Combustion Instability
Applied Mechanics and Materials, 2014In the present paper, a combined method of large eddy simulations for non-premixed combustion in a turbulent flow coupled with proper orthogonal decomposition of instantaneous velocity, pressure and temperature fields is developed in order to identify the effect of coherent structure and to obtain a reduced order model for control model.
Sterian Danaila, Constantin Leventiu
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AIAA Journal, 1974
THE following equations governing the phenomenon of intrinsic instability of combustion, leading to low frequency oscillations in a rocket motor using a single liquid propellant, were derived and investigated by L. Crocco.
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THE following equations governing the phenomenon of intrinsic instability of combustion, leading to low frequency oscillations in a rocket motor using a single liquid propellant, were derived and investigated by L. Crocco.
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