ISABE – 50 Years Revolution....again!
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1223, doi. 10.1017/aer.2022.76
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- Article
Works matching IS 00019240 AND DT 2022 AND VI 126 AND IP 1302
Results: 13
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An altitude capable rig for studying engine inlet velocity profile effects: Boundary layer generator.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1430, doi. 10.1017/aer.2022.67
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- Article
3
Identification and classification of operating flow regimes and prediction of stall in a contra-rotating axial fan using machine learning.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1351, doi. 10.1017/aer.2022.63
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- Article
4
Impact of tank gravimetric efficiency on propulsion system integration for a first-generation hydrogen civil airliner.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1324, doi. 10.1017/aer.2022.60
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5
On the effect of inter compressor duct length on compressor performance.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1333, doi. 10.1017/aer.2022.51
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- Article
6
Sand erosion modeling in generic compressor rig testing.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1303, doi. 10.1017/aer.2022.41
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- Article
7
Numerical investigations on the effect of blade tip winglet on leakage flow loss reduction for a zero inlet swirl turbine rotor.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1370, doi. 10.1017/aer.2022.6
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8
Effects of flame-flame interaction on emission characteristics in gas turbine combustors.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1414, doi. 10.1017/aer.2022.37
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- Article
9
Design of a sub-scale fan for a boundary layer ingestion test with by-pass flow.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1288, doi. 10.1017/aer.2022.28
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- Article
10
Performance of a turbojet engine with fluidic thrust vectoring.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1225, doi. 10.1017/aer.2022.27
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- Article
11
Aeroengine transient performance simulation integrated with generic heat soakage and tip clearance model.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1265, doi. 10.1017/aer.2022.15
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- Article
12
Investigation on shock-induced separation loss mitigation method considering radial equilibrium in a transonic compressor rotor.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1394, doi. 10.1017/aer.2022.14
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- Article
13
Multidisciplinary conceptual design for a hybrid-electric commuter aircraft.
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- Aeronautical Journal, 2022, v. 126, n. 1302, p. 1242, doi. 10.1017/aer.2022.32
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- Article