Results 151 to 160 of about 678 (224)

Study on jet dynamic impact performance under the influence of standoff. [PDF]

Sci Rep
Wang Y, Yin J, Zhang X, Yi J, Li X.
europepmc   +1 more source

Experimental Evaluation of High-Purity-Silica Reinforced Ablative Composites As Nozzle Sections of 7.8-Inch-(19.8 CM) Diameter Throat Storable-Propellant Rocket Engine.

, 1967
Donald A. Peterson
openalex   +1 more source

Sustainable Design and Wall Thickness Optimization for Enhanced Lifetime of Ultra-High Temperature Ceramic Matrix Composite Thruster for Use in Green Propulsion Systems. [PDF]

Materials (Basel)
Doozandeh T, Jindal P, Botchu J.
europepmc   +1 more source

Numerical analysis of over-expansion rocket engine nozzles

, 2015
Kim, Hyoung Chol, 中橋 和博, Shigeru Obayashi, 中橋 和博, 大林 茂, 大林　茂   +5 more
openalex   +1 more source

Numerical Simulation of Fluid-Structure Interaction for Thermochemical Ablation of Solid Rocket Engine Nozzle

Zhitan Zhou, Dehua Cao, Ranhui Liang
openalex   +1 more source

659 Enhancement of Rocket Engine Thrust using Variable Area Ratio Nozzle

, 2008
Naoyuki Otsubo, Kunio Hirata, Hirotaka Otsu   +2 more
openalex   +1 more source

Vibration Control of Flexible Launch Vehicles Using Fiber Bragg Grating Sensor Arrays. [PDF]

Sensors (Basel)
van der Veek B, Gutierrez H, Wise B, Kirk D, van Barschot L.   +4 more
europepmc   +1 more source

Study on the Particle Deposition Characteristics of Transpiration Cooling Structures with Sintered Wire Mesh. [PDF]

Micromachines (Basel)
Zhang Z, Luo X, Peng Y.
europepmc   +1 more source