Works matching DE "ROCKET engine combustion"
Results: 19
Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 6, p. 652, doi. 10.1134/S0010508217060053
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- Article
Diagnostics of acoustic properties of the combustion zone by means of periodic changes in the nozzle throat area.
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- Combustion, Explosion, & Shock Waves, 2008, v. 44, n. 6, p. 627, doi. 10.1007/s10573-008-0096-8
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- Article
Thermal Decomposition and Combustion of Ammonium Dinitramide (Review).
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- Combustion, Explosion, & Shock Waves, 2005, v. 41, n. 6, p. 657, doi. 10.1007/s10573-005-0079-y
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- Article
Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 332, doi. 10.2322/tjsass.59.332
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- Article
Thermodynamic substantiation of the existence of a phase transition point with a change in the structure of the solid-fuel mixture glycidyl azide Polymer/RDX.
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- Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 5, p. 1058, doi. 10.1007/s10891-012-0747-1
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- Article
Design optimization of a methane-fuel rocket combustor with a genetic algorithm.
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- Journal of Mechanical Science & Technology, 2015, v. 29, n. 4, p. 1457, doi. 10.1007/s12206-015-0318-4
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- Article
Flight Overloading Effect on the Working-Process Instability in the Combustion Chamber of a Solid-Fuel Rocket Engine.
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- Doklady Physics, 2004, v. 49, n. 9, p. 527, doi. 10.1134/1.1810579
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- Article
Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability.
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- Energies (19961073), 2015, v. 8, n. 2, p. 1195, doi. 10.3390/en8021195
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- Article
Mechanical Properties of Gel Propellants with Nanoparticles.
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- Journal of Energetic Materials, 2004, v. 22, n. 2, p. 69, doi. 10.1080/07370650490492824
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- Article
Contact diagnostics of combustion products of rocket engines, their units, and systems.
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- Solar System Research, 2013, v. 47, n. 7, p. 582, doi. 10.1134/S0038094611070094
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- Article
Analysis of Coolant Mass Flow Requirements for Transpiration Cooled Ceramic Thrust Chambers.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 31
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- Article
Combustion Phenomena within a RBCC Engine under Scramjet-mode Operation.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 71
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- Article
Numerical Study of Real Gas Effects on Shock Tube Problems at Supercritical Conditions.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 39
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- Article
A Study on Combustion Efficiency Improvement of Low Melting Temperature Thermoplastics as a Hybrid Rocket Fuel.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 9
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- Article
Development and Ground Combustion Test of a Subscale Reusable Winged Rocket.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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- Article
373. INFLUENCE OF OVERLOAD ON LOW-FREQUENCY INSTABILITY OF WORKING PROCESS IN THE COMBUSTION CHAMBER OF THE SOLID PROPELLANT ROCKET ENGINE.
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- Journal of Vibroengineering, 2008, v. 10, n. 3, p. 272
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- Article
International symposium on thermoacoustic instabilities in gas turbines and rocket engines: Industry meets academia.
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- 2017
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- Publication type:
- Proceeding
The use of OH* and CH* as heat release markers in combustion dynamics.
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- International Journal of Spray & Combustion Dynamics, 2017, v. 9, n. 4, p. 409, doi. 10.1177/1756827717718483
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- Article
Determination of a Two Variable Approximation Function with Application to the Fuel Combustion Charts.
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- INCAS Bulletin, 2017, v. 9, n. 3, p. 3, doi. 10.13111/2066-8201.2017.9.3.1
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- Article