Results 141 to 150 of about 678 (224)

Advanced Thermal Protection Systems Enabled by Additive Manufacturing of Hybrid Thermoplastic Composites. [PDF]

Polymers (Basel)
Badea TA, Crisan AA, Maier LR.
europepmc   +1 more source

Investigation of unswept ramp system with lobe shape nozzle for fuel mixing of hydrogen jet at a scramjet engine. [PDF]

Sci Rep
Omar I, El-Sharkawy MR, Ahmed M, Singh PK, Rajab H, Ali R, Ali NB, Rajhi W, Said LB, Abodollahi SA.   +9 more
europepmc   +1 more source

Opposition-based chaotic evolution for optimization. [PDF]

Sci Rep
Li T, Pei Y.
europepmc   +1 more source

An experimental method of determining the mean heat transfer coefficient for the nozzle of a solid propellant rocket engine, by means of constant flow calorimetry

, 1962
A.G. Smith, T. A. Carberry
openalex   +1 more source

Transient spray combustion characteristics in a gas-liquid pintle rocket engine under acoustic excitation. [PDF]

Sci Rep
Jin X, Zhu C, Chen D, Zhang Z.
europepmc   +1 more source

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

, 2013
Y. I. Ageenko, V. E. Nigodyuk, V. V. Ryzhkov, А. В. Сулинов, С. А. Шустов   +4 more
openalex   +2 more sources

Multi-Scale Mechanical Characterization of Additively Manufactured GRCop-42 and GRCop-84 Alloys. [PDF]

JOM (1989)
Mahtabi M, Roshan M, Demeneghi G, Gradl P, Bednarczyk W, Cios G, Haghshenas M.   +6 more
europepmc   +1 more source

Particle-Filter-Based Fault Diagnosis for the Startup Process of an Open-Cycle Liquid-Propellant Rocket Engine. [PDF]

Sensors (Basel)
Cha J, Ko S, Park SY.
europepmc   +1 more source

Investigation of the gas flow features in the path of a rocket engine with a swinging nozzle

A. A. Shumikhin, М. Р. Королева   +1 more
openalex   +1 more source