Results 161 to 170 of about 10,699 (233)

Synthesis, Structure, Properties, and Applications of Fluorinated Polyurethane. [PDF]

Polymers (Basel)
Li D, Yu L, Lu Z, Kang H, Li L, Zhao S, Shi N, You S.   +7 more
europepmc   +1 more source

Effects of Thermal Damage on Impact Response Characteristics of High-Energy Propellants. [PDF]

Polymers (Basel)
Guo F, Nie J, Zhang S, Liang J, Liu R, Zou Y, Han Y.   +6 more
europepmc   +1 more source

Surface interactions and radical generation in TCD decomposition: a DFT approach. [PDF]

J Mol Model
Knoth SE, Tunega D, Aquino AJA.
europepmc   +1 more source

Enhancing the landing guidance of a reusable launch vehicle by improving genetic algorithm-based deep reinforcement learning using Hybrid Deterministic-Stochastic algorithm. [PDF]

PLoS One
Nugroho L, Andiarti R, Akmeliawati R, Wijaya SK.   +3 more
europepmc   +1 more source

Combustion Enhancement of Gel Propellant Containing High Concentration Aluminum Particles Based on Carbon Synergistic Effect. [PDF]

Gels
Chen J, Zhao H, Li W, Liu H.
europepmc   +1 more source

Research progress on the catalytic and thermal decomposition of ammonium dinitramide (ADN). [PDF]

RSC Adv
Tian Y, Xu W, Cong W, Bi X, He J, Song Z, Guan H, Huang C, Wang X.   +8 more
europepmc   +1 more source

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Liquid-Propellant Rocket Engine Injector Dynamics

Journal of Propulsion and Power, 1998
The dynamic characteristics of liquid-rocket injectors in the presence of intense combustion-chamber and propellant feed-line oscillations are discussed. Liquid-propellant injectors always function in nonsteady e ow environments and are therefore considered as a dynamic component of an engine.
Vladimir G. Bazarov, Vigor Yang
openaire   +1 more source

Simulation of liquid propellant rocket engine combustion instabilities

17th Aerospace Sciences Meeting, 1979
A simulation technique for studying the high frequency combustion instabilities of liquid propellant rocket engines has been developed and used to investigate various aspects of instability phenomena. Of importance was investigation of the significance of the method of coupling the combustion and the gas dynamics of the system.
M. B. Ventrice, J. C. Fang, K. R. Purdy
openaire   +1 more source

Propellant Injector Influence on Liquid-Propellant Rocket Engine Instability

Journal of Propulsion and Power, 2015
The avoidance of acoustic instabilities, which may cause catastrophic failure, is demanded for liquid-propellant rocket engines. This occurs when the energy released by combustion amplifies acoustic disturbances; it is therefore essential to avoid such positive feedback.
Pavel P. Popov, William A. Sirignano, Athanasios Sideris   +2 more
openaire   +1 more source