Unified approach for conjugate heat-transfer analysis of high speed air flow through a water-cooled nozzle.
- Published in:
- Aeronautical Journal, 2016, v. 120, n. 1224, p. 355, doi. 10.1017/aer.2015.15
- By:
- Publication type:
- Article
Works matching DE "LIQUID propellant rocket engines"
Results: 24
1
2
Testing thick nickel coatings applied on two-layer (nonferromagnet-ferromagnet) bases by magnetodynamic thickness gauges.
- Published in:
- Russian Journal of Nondestructive Testing, 2014, v. 50, n. 4, p. 187, doi. 10.1134/S1061830914040044
- By:
- Publication type:
- Article
3
New preliminary design method of pump-fed system in a cryogenic lpre base on gradient and genetic algorithms.
- Published in:
- Modares Mechanical Engineering, 2015, v. 15, n. 5, p. 71
- By:
- Publication type:
- Article
4
Levitation force of small clearance superconductor-magnet system under non-coaxial condition.
- Published in:
- Modern Physics Letters B, 2017, v. 31, n. 8, p. -1, doi. 10.1142/S0217984917500750
- By:
- Publication type:
- Article
5
Development Status of L75: A Brazilian Liquid Propellant Rocket Engine.
- Published in:
- Journal of Aerospace Technology & Management, 2014, v. 6, n. 4, p. 475, doi. 10.5028/jatm.v6i4.386
- By:
- Publication type:
- Article
6
The duration of non-stationary transitional periods in vacuum systems for mass spectrometric inspection of the leaktightness of large objects in rocket and space systems.
- Published in:
- Welding International, 2017, v. 31, n. 6, p. 462, doi. 10.1080/09507116.2016.1268764
- By:
- Publication type:
- Article
7
Formation of cracks in EP202 and EK61 alloys in welding of structures of liquid rocket engines.
- Published in:
- Welding International, 2013, v. 27, n. 2, p. 159, doi. 10.1080/09507116.2012.695550
- By:
- Publication type:
- Article
8
Numerical analysis of reactive turbulent flow in the thrust chamber of RD-108 engine rocket.
- Published in:
- Defence Technology, 2019, v. 15, n. 4, p. 565, doi. 10.1016/j.dt.2018.12.004
- By:
- Publication type:
- Article
9
Application and Comparison of Different Combustion Models of High Pressure LO<sub>X</sub> /CH<sub>4</sub> Jet Flames.
- Published in:
- Energies (19961073), 2014, v. 7, n. 1, p. 477, doi. 10.3390/en7010477
- By:
- Publication type:
- Article
10
Intensification of Heat Exchange in the Regenerative Cooling System of a Liquid-Propellant Rocket Engine.
- Published in:
- Journal of Engineering Physics & Thermophysics, 2018, v. 91, n. 3, p. 601, doi. 10.1007/s10891-018-1781-4
- By:
- Publication type:
- Article
11
Concerning the problem of dynamic damping of the vibration combustion self-oscillations in a liquid-propellant rocket engine.
- Published in:
- Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 6, p. 1346, doi. 10.1007/s10891-012-0781-z
- By:
- Publication type:
- Article
12
Investigations of Rubbing Phenomenon During Coast-Up Operation of a Cryogenic Engine Turbopump.
- Published in:
- Journal of Vibration Engineering & Technologies, 2020, v. 8, n. 5, p. 737, doi. 10.1007/s42417-019-00181-6
- By:
- Publication type:
- Article
13
Air-Breathing Ramjet Electric Propulsion for Controlling Low-Orbit Spacecraft Motion to Compensate for Aerodynamic Drag.
- Published in:
- Solar System Research, 2017, v. 51, n. 7, p. 639, doi. 10.1134/S0038094617070048
- By:
- Publication type:
- Article
14
An Experiment on Cavitating Flow in Rocket Engine Inducer.
- Published in:
- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 2, p. 306, doi. 10.16356/j.1005-1120.2019.02.013
- By:
- Publication type:
- Article
15
Molecular Dynamics Simulation of a Jet in a Binary System at Supercritical Environment.
- Published in:
- Molecules, 2019, v. 24, n. 1, p. 31, doi. 10.3390/molecules24010031
- By:
- Publication type:
- Article
16
NUMERICAL INVESTIGATION OF SWIRL INJECTOR LOX/GH<sub>2</sub> RATIO INFLUENCE OVER COMBUSTION CONDITIONS INTO A LIQUID ROCKET ENGINE.
- Published in:
- Annals (Constanţa Maritime University), 2011, v. 11, n. 14, p. 67
- By:
- Publication type:
- Article
17
Experimental Investigation of Transient Forced Convection of Liquid Methane in a Channel at High Heat Flux Conditions.
- Published in:
- Experimental Heat Transfer, 2016, v. 29, n. 1, p. 97, doi. 10.1080/08916152.2014.945052
- By:
- Publication type:
- Article
18
NDT INFO.
- Published in:
- 2017
- Publication type:
- Abstract
19
Laser ultrasonic method for the defectoscopy of soldered joints of liquid-propellant rocket engines.
- Published in:
- Insight: Non-Destructive Testing & Condition Monitoring, 2015, v. 57, n. 4, p. 201, doi. 10.1784/insi.2015.57.4.201
- By:
- Publication type:
- Article
20
Contact diagnostics of combustion products of rocket engines, their units, and systems.
- Published in:
- Solar System Research, 2013, v. 47, n. 7, p. 582, doi. 10.1134/S0038094611070094
- By:
- Publication type:
- Article
21
Numerical analysis of the thermal characteristics of a gas-dynamic ignition system.
- Published in:
- Journal of Mechanical Science & Technology, 2018, v. 32, n. 5, p. 2385, doi. 10.1007/s12206-018-0450-z
- By:
- Publication type:
- Article
22
Development of a system analysis program for a liquid rocket engine.
- Published in:
- Journal of Mechanical Science & Technology, 2015, v. 29, n. 6, p. 2375, doi. 10.1007/s12206-015-0535-x
- By:
- Publication type:
- Article
23
Feasibility Study on Additive Manufacturing of Liquid Rocket Combustion Chamber.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2018, v. 16, n. 3, p. 261, doi. 10.2322/tastj.16.261
- By:
- Publication type:
- Article
24
Numerical Study of Real Gas Effects on Shock Tube Problems at Supercritical Conditions.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 39
- By:
- Publication type:
- Article