Application of a Liquid Propellant Rocket as a Turbojet Thrust Augmentation SystemRamjet enginesLiquid propellant rocket enginesThrustAugmentationControl systemsRocket ramjetsNo abstract available.Scott, J. E.Princeton Univ.
A nonlinear analysis of the stability of longitudinal combustion-driven oscillations in liquid propellant rocket motors is presented. A modified version of the Galerkin method is used to obtain solutions valid for moderate amplitude instabilities in rocket combustors having a low Mach number mean flow....
1) application of enamel,enamelling 涂搪例句>> 2) enamel coating 搪瓷涂层 1. Research on nano-composite enamel coatings for liquid propellant rocket engine; 纳米复合搪瓷涂层在液体火箭发动机的应用研究 2. An enamel glaze that containing cerium oxide was deposited on titanium alloys using ...
The authors would like to thank Sergio Tuset (CEO of Condorchem Envitech, S.L.) for sponsoring personally the associated research project.References (22) A. Ulas Passive flow control in liquid-propellant rocket engines with cavitating venturi Flow Meas. Instrum. (2006) A.M. Abdulaziz ...
Gelled propellant Rocket Motors combine excellent thrust control with a very low hazard potential and are as environmentally friendly as liquid propellants can be that can be stored at ambient condition. The paper gives a brief descripti... KW Naumann,PC Pinto,J Ramsel,... - Aiaa/sae/asee Joi...
LIQUID PROPELLANT PULSED PLASMA THRUSTER ∗ Liquid propellant is different from gaseous propellant with respect to the following points. First, liquid injected into the vacuum diffuses more slowly than gas, and there is no need of fast acting valve. For instance, the calculation o... Koizumi,...
A third order theory is developed to predict the nonlinear behavior of unstable liquid-propellant rocket engines. The stability of a cylindrical combustor with a distributed steady state combustion process and a multi-orifice quasi-stead... AIAA - 《Combustion Science & Technology》 被引量: 8发表...
C., Yang, V.: Comprehensive review of liquid-propellant combustion instabilities in F-1 engines. J. Propul. Power 9, 657–677 (1993) Article Google Scholar Scalo, C., Bodart, J., Lele, S. K.: Compressible turbulent channel flow with impedance boundary conditions. Phys. Fluids 27, ...
Application of Combustion Stabilization Devices to Liquid Rocket Engine Application of combustion stabilization devices such as baffle and acoustic cavity to liquid propellant rocket engine is investigated to suppress high-frequency combustion instability, i.e., acoustic instability. First, these damping dev...
Hydrogen storage and transportation is the most critical link and the bottleneck of hydrogen energy layout in China. In the next decade, high-pressure gaseous and cryogenic liquid hydrogen will remain the primary storage and transportation methods. Therefore, it is essential to keep abreast of the ...