WAKE INGESTION PROPULSION BENEFIT

被引:174
|
作者
SMITH, LH
机构
[1] GE Aircraft Engines, Cincinnati, OH
关键词
D O I
10.2514/3.11487
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
It is well-known that the efficiency of propulsion is improved if part or all of the propulsive fluid comes from the wake of the craft being propelled. In this article this propulsion benefit is quantified in terms of wake parameters and propulsor properties. The formulations apply directly to unducted fans or propellers, but the conclusions are also relevant to ducted propulsors. It is found that the power saving is greatest when the propulsor disk loading is high, when the wake form factor is high (flow near separation), and when the propulsor design is such that the wake profile tends to be flattened as it passes through the propulsor (high wake recovery). Examples are given showing that the benefit can be in the 20% range in some cases. Propeller design parameters that lead to high wake recovery are also given.
引用
收藏
页码:74 / 82
页数:9
相关论文
共 50 条
  • [41] Performance analysis of turbo-electric propulsion system with fuselage boundary layer ingestion
    Samuelsson, Sebastian
    Gronstedt, Tomas
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 109 (109)
  • [42] TURBOELECTRIC DISTRIBUTED PROPULSION MODELLING ACCOUNTING FOR FAN BOUNDARY LAYER INGESTION AND INLET DISTORTION
    Athanasakos, Georgios
    Aretakis, Nikolaos
    Alexiou, Alexios
    Mathioudakis, Konstantinos
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 5, PT II, 2020,
  • [43] Numerical investigation on the effects of boundary layer ingestion on aerodynamic performance of distributed propulsion system
    Cui, Rong
    Pan, Tianyu
    Li, Qiushi
    Zhang, Jian
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 33 (05): : 1076 - 1083
  • [44] Towards More Efficient Electric Propulsion UAV Systems Using Boundary Layer Ingestion
    Arias, Jonathan
    Martinez, Francisco
    Cando, Edgar
    Valencia, Esteban
    Gonzalez-Aguilera, Diego
    DRONES, 2023, 7 (12)
  • [45] Aerodynamic Performance of an Aircraft with Aft-Fuselage Boundary-Layer-Ingestion Propulsion
    Della Corte, Biagio
    van Sluis, Martijn
    Rao, Arvind Gangoli
    Veldhuis, Leo L. M.
    JOURNAL OF AIRCRAFT, 2022, 59 (04): : 1054 - 1070
  • [46] SOME CONTRIBUTIONS TO PROPULSION THEORY - NONISENTROPIC DUCT FLOW AND THE GENERAL DRAG WAKE TRAVERSE
    BORE, CL
    AERONAUTICAL JOURNAL, 1993, 97 (965): : 177 - 178
  • [47] Effect of input perturbation on the performance and wake dynamics of aquatic propulsion in heaving flexible foils
    Lehn, Andrea M.
    Thornycroft, Patrick J. M.
    Lauder, George V.
    Leftwich, Megan C.
    PHYSICAL REVIEW FLUIDS, 2017, 2 (02):
  • [48] ADJOINT AFTSHIP RE-DESIGN FOR WAKE OPTIMISATION UNDER THE INFLUENCE OF ACTIVE PROPULSION
    Kroeger, J.
    Stueck, A.
    Rung, T.
    COMPUTATIONAL METHODS IN MARINE ENGINEERING IV (MARINE 2011), 2011, : 626 - 637
  • [49] Numerical research on mechanism of the effect of propeller shaft brackets on wake field and propulsion performance
    Cui, Lianzheng
    Chen, Zuogang
    Qin, Jiangtao
    Zhou, Lilan
    OCEAN ENGINEERING, 2021, 228
  • [50] Propulsion Performance and Wake Dynamics of Heaving Foils under Different Waveform Input Perturbations
    Gao, Pengcheng
    Huang, Qiaogao
    Pan, Guang
    JOURNAL OF MARINE SCIENCE AND ENGINEERING, 2021, 9 (11)