Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]
Materials (Basel)Gržetić J +6 more
europepmc +1 more source
Numerical Investigation of Transonic Flow-Induced Spontaneous Condensation in Micro-Ejector Nozzles. [PDF]
Micromachines (Basel), 2023 Han Y, Wang X, Wang W, Lee YX, Li A.
europepmc +1 more source
Development and demonstration of flueric sounding rocket motor ignition [PDF]
An analytical and experimental program is described which established a flueric rocket motor ignition system concept incorporating a pneumatic match with a simple hand pump as the only energy source.
Marchese, V. P.
core +1 more source
Influence of plasma-enhanced combustion on RBCC engine using URANS. [PDF]
Sci RepZhang WR, Liu YS, Zou XR, Xu C, Xue R.
europepmc +1 more source
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle [PDF]
A 1030:1 carbon steel, heat-sink nozzle was tested. The test conditions included a nominal chamber pressure of 2413 kN/sq m and a mixture ratio range of 2.78 to 5.49. The propellants were gaseous oxygen and gaseous hydrogen.
Kacynski, Kenneth J. +2 more
core +1 more source
Experimental Study of Flame Dynamics in a Triple-Injector Swirling Nonpremixed Combustor Under Different Thermoacoustic Self-Excited Instability Modes. [PDF]
Sensors (Basel)Zhang X, Wang S, Liu Y.
europepmc +1 more source
Design, fabrication and evaluation of tungsten encapsulated silver infiltrated porous tungsten rocket nozzle inserts Final report [PDF]
Rocket nozzle throat insert encapsulated in solid tungsten ...
Price, J.
core +1 more source
Cf/SiC Ceramic Matrix Composites with Extraordinary Thermomechanical Properties up to 2000 °C. [PDF]
Nanomaterials (Basel), 2023 Park MS +5 more
europepmc +1 more source
Determination of the effects of nozzle nonlinearities upon nonlinear stability of liquid propellant rocket motors [PDF]
The research is reported concerning the development of a three-dimensional nonlinear nozzle admittance relation to be used as a boundary condition in the nonlinear combustion instability theories for liquid propellant rocket engines.
Padmanabhan, M. S. +2 more
core +1 more source
Study on Graphene-Reinforced Epoxy Solvent-Borne High-Temperature-Resistant Adhesives for Bonding C/C Composites Under Extreme Temperatures. [PDF]
Materials (Basel)Wang Y +6 more
europepmc +1 more source