Works matching DE "COMBUSTION chambers in aircraft gas turbines"
Results: 10
EXERGETIC ANALYSIS OF AN AIRCRAFT TURBOJET ENGINE WITH AN AFTERBURNER.
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- Thermal Science, 2013, v. 17, n. 4, p. 1181, doi. 10.2298/TSCI110911043E
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- Article
Detailed and Reduced Mechanisms of Jet a Combustion at High Temperatures.
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- Combustion Science & Technology, 2008, v. 180, n. 10/11, p. 1788, doi. 10.1080/00102200802258379
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- Article
ACTIVE INSTABILITY CONTROL EFFECTIVENESS IN A LIQUID FUELED COMBUSTOR.
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- Combustion Science & Technology, 2006, v. 178, n. 7, p. 1251, doi. 10.1080/00102200500297042
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- Article
Numerical Investigation of the Effects of Biofuel Characteristics on the Injector Nozzle Erosion Process.
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- Tribology Transactions, 2013, v. 56, n. 2, p. 161, doi. 10.1080/10402004.2012.709918
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- Article
HOLE MAKING IN GAMMA TIAL.
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- DAAAM International Scientific Book, 2010, p. 337, doi. 10.2507/daaam.scibook.2010.32
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- Article
GE Rolls-Royce fighter engine team hits afterburner on third new JSF engine.
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- Asia-Pacific Defence Reporter, 2010, v. 36, n. 3, p. 8
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- Article
EL DIABLO.
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- Leonardo, 2007, v. 40, n. 4, p. 343
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- Article
Effect of Surface Tension and Evaporation on Phase Change of Fuel Droplets.
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- Heat Transfer Engineering, 2001, v. 22, n. 3, p. 33, doi. 10.1080/014576301300092568
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- Article
The aerodynamic challenges of aeroengine gas-turbine combustion systems.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 557, doi. 10.1017/S0001924000009386
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- Article
Cold flow analysis of trapped vortex combustor using two equation turbulence models.
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- Aeronautical Journal, 2008, v. 112, n. 1136, p. 569, doi. 10.1017/S0001924000002530
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- Article