Results 11 to 20 of about 349,167 (288)
A survey of inlet/engine distortion compatibility [PDF]
19th Joint Propulsion Conference, 1983 The history of distortion analysis is traced back to its origin in parallel compressor theory which was initially proposed in the late fifties. The development of this theory is reviewed up to its inclusion in the complex computer codes of today.
D. BOWDITCH, R. COLTRIN
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Turboelectric Distributed Propulsion System Modelling [PDF]
, 2013 The Blended-Wing-Body is a conceptual aircraft design with rear-mounted, over wing engines. Turboelectric distributed propulsion system with boundary layer ingestion has been considered for this aircraft.
Liu, Chengyuan
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Modelling & integration of advanced propulsion systems [PDF]
, 2008 This research study focuses on the design of advanced propulsion cycles, having as primary design goal the improvement on noise emissions and fuel consumption.
Doulgeris, Georgios C.
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Influence of inlet distortion on fan aerodynamic performance [PDF]
, 2019 Inlet distortion can lead to loss in efficiency and stability margin of the fan which in return jeopardises flight safety. These aspects driven by inlet distortion are becoming increasingly challenging for the designers of next-generation turbofan engines. With the increase of computational capability and improvements in numerical models, computational
Zhang, Wenqiang
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Energies, 2023 Although inlet bent pipes are usually adopted due to limited installation space, the influences of different bend pipes on the inlet flow characteristics and performance of centrifugal compressors are still unclear.
Xing Li +6 more
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An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor
International Journal of Rotating Machinery, 2005 An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with
Eddie Yin-Kwee Ng +3 more
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Effect of inlet distortion with crosswind on aircraft-engine intake aerodynamic performance
Nihon Kikai Gakkai ronbunshu, 2022 This paper describes an experimental study on inlet distortion in the flow ingested to an intake of a ducted fan. Recent high bypass ratio engines tend to shorten the nacelle length for better fuel consumption.
Hiroki NARUSE +7 more
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Analysis of Flow Field Distortion in Ship Inlet System and Its Effect on Compressor Performance [PDF]
Journal of Applied Fluid Mechanics, 2023 Intake system structure design is categorized under gas turbine marine technology, and its performance affects the inlet flow field of the compressor, thereby impacting the overall operation stability of the gas turbine.
Z. Y. Wang, C. X. He, Y. L. Qu
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Applied Sciences, 2023 Submerged inlet has been widely used in UAVs and cruise missiles due to its good stealth characteristics, but it also brings the disadvantage of poor aerodynamic characteristics.
Junyao Zhang, Baigang Mi
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Effect of Fan on Inlet Distortion: Mixed-Fidelity Approach [PDF]
AIAA Journal, 2018 Inlet distortion is typically encountered during off-design conditions on civil aircraft and in S-ducts in military aircraft. It is known to cause severe deterioration to the performance of a gas-turbine engine. As intakes become shorter, there is an increased interaction between the inlet distortion and the downstream fan.
Ma, Y +3 more
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