MainCatalogAviation and Rocket-Space EngineeringThermal, Electric Jet Engines, and Power Plants of Aircrafts
Usage of oxygen-and-methane propellant in liquid-propellant rocket engines
| Authors: Bregvadze D.T., Gabidulin O.V., Gurkin A.A., Zabolotko I.A. | Published: 29.11.2017 |
| Published in issue: #12(17)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-12-205 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid-propellant rocket engines, liquid methane, prospective rocket fuel, cooling of rocket engine, fuel-to-oxidizer ratio | |
Investigating the thermohydraulic efficiency of the liquid-propellant rocket engine porous tract of cooling with the interchannel coolant flow
| Authors: Anfimov M.V. | Published: 17.10.2017 |
| Published in issue: #10(15)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-10-188 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: Thermohydraulic efficiency, porous tract, liquid-propellant rocket engine cooling, thermal protection | |
Simulating the process of cooling the high temperature flow in experimental ground rigs by means of water injection
| Authors: Polyakov K.V. | Published: 04.10.2017 |
| Published in issue: #10(15)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-10-181 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: split, diffusion, disintegration model, cooling the high temperature flow | |
Numerical simulation of combustion processes for hydrogen-air mixture in a variable cross-section pipe
| Authors: Korshunova M.R. | Published: 14.09.2017 |
| Published in issue: #9(14)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-9-165 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: combustion, hydrogen-air mixture, gas dynamic computation, simulation of combustion in a pipe, reactor-based approach | |
Standard parameters calculation in experimental investigations of characteristic features of ignition and combustion of boron-containing combustible particles conglemerates
| Authors: Ryazanov R.S., Sumnitel’nyy N.V. | Published: 19.04.2017 |
| Published in issue: #3(8)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-3-86 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: conglomerate, Bunsen burner, mass flow, oxidizer excess ratio, check valve, flame flow rate | |