[1] A. K, G. W. Innovation for sustainable aviation in a global environment [M/OL]. 2012[
[2] M K, L L. European aviation environmental report 2016 [R], 2016.
[3] SUDER K L, DELAAT J, HUGHES C, et al. NASA environmentally responsible aviation project’s propulsion technology phase i overview and highlights of accomplishments [Z]. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2013
[4] SUDER K L. Overview of the nasa environmentally responsible aviation project’s propulsion technology portfolio [Z]. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2012
[5] MOIROU N G M, SANDERS D S, LASKARIDIS P. Advancements and prospects of boundary layer ingestion propulsion concepts [J]. Progress in Aerospace Sciences, 2023, 138.
[6] HALL C A, CRICHTON D. Engine design studies for a silent aircraft [J]. Journal of Turbomachinery, 2007.
[7] FLOREA R V, MATALANIS C, HARDIN L W, et al. Parametric analysis and design for embedded engine inlets [J]. Journal of Propulsion and Power, 2015, 31(3): 843-50.
[8] HALL D K, HUANG A C, URANGA A, et al. Boundary layer ingestion propulsion benefit for transport aircraft [J]. Journal of Propulsion and Power, 2017, 33(5): 1118-29.
[9] LIEBECK R H. Design of the blended wing body subsonic transport [J]. Journal of Aircraft, 2004, 41(1): 10-25.
[10] SMITH A M O, ROBERTS H E. The jet airplane utilizing boundary layer air for propulsion [J]. Journal of the Aeronautical Sciences, 1947, 14(2): 97-109.
[11] THURSTON S, EVANBAR M S. Efficiency of a propulsor on a body of revolution-inducting boundary-layer fluid [J]. Journal of Aircraft, 1966, 3(3): 270-7.
[12] WISLICENUS G F. Hydrodynamics and propulsion of submerged bodies [J]. ARS Journal, 1960, 30(12): 1140-8.
[13] BRANDAU J H. Performance of waterjet propulsion systems- a review of the state-of-the-art [J]. Journal of Hydronautics, 1968, 2(2): 61-73.
[14] LYNCH F. A theoretical investigation of the effect of ingesting airframe boundary layer air on turbofan engine fuel consumption [J]. 1960.
[15] DOUGLASS W. Propulsive efficiency with boundary-layer ingestion [R], 1970.
[16] SMITH L H. Wake ingestion propulsion benefit [J]. Journal of Propulsion and Power, 1993, 9(1): 74-82.
[17] BERRIER B L, MOREHOUSE M B. Evaluation of flush-mounted, s-duct inlets with large amounts of boundary layer ingestion [R], 2003.
[18] LIU L, LI G, WANG B, et al. Suction control of a boundary layer ingestion inlet [J]. Aerospace, 2023, 10(12).
[19] 巍 魏, 任思源, 达兴亚. 边界层吸入对方转圆进气道、风扇耦合影响 [J]. 航空动力学报, 2020, 35(9): 1943-5.
[20] PLAS A, CRICHTON D, SARGEANT M, et al. Performance of a boundary layer ingesting (bli) propulsion system [Z]. 45th AIAA Aerospace Sciences Meeting and Exhibit. 2007.10.2514/6.2007-450
[21] CELESTINA M L, LONG-DAVIS M J. Large-scale boundary layer ingesting propulsor research [Z]. 2019
[22] FELDER J L, TONG M T, SCHNULO S L, et al. Updated assessment of turboelectric boundary layer ingestion propulsion applied to single-aisle commercial transport [R], 2022.
[23] BLUMENTHAL B T, ELMILIGUI A A, GEISELHART K A, et al. Computational Investigation of a Boundary-Layer-Ingestion Propulsion System [J]. Journal of aircraft, 2018, 55(3): 1141-53.
[24] DIAMANTIDOU D E, HOSAIN M L, KYPRIANIDIS K G. Recent advances in boundary layer ingestion technology of evolving powertrain systems [J]. Sustainability, 2022, 14(3).
[25] 达兴亚, 范召林, 熊能, et al. 分布式边界层吸入推进系统的建模与分析 [J]. 航空学报, 2018, 39(7): 122048.
[26] 汪昆. 狭缝式边界层吸入进气道的流动机理与畸变抑制研究 [D]. 南京; 南京航空航天大学, 2024.
[27] 陈逖, 邱名, 江雄. 边界层吸入式推进系统研究进展[Z].（第三届）中国航空科学技术大会. 北京. 2017
[28] WELSTEAD J R, FELDER J L. Conceptual design of a single-aisle turboelectric commercial transport with fuselage boundary layer ingestion [Z]. 54th AIAA Aerospace Sciences Meeting. San Diego, CA. 2016
[29] BERRIER B L, CARTER M B, BRIAN G A. High reynolds number investigation of a flush-mounted, s-duct inlet with large amounts of boundary layer ingestion [R]. Hampton, Virginia: Langley Research Center,NASA, 2005.
[30] 陈健华. 附面层吸入式进气道主动流动控制研究 [D]. 哈尔滨; 哈尔滨工业大学, 2009.
[31] LEE C, BOEDICKER C. Subsonic diffuser design and performance for advanced fighter aircraft [Z]. Aircraft Design Systems and Operations Meeting. 1985.10.2514/6.1985-3073
[32] CHIANG C, KOO D, ZINGG D W. Aerodynamic shape optimization of an s-duct intake for a boundary-layer ingesting engine [J]. Journal of Aircraft, 2022, 59(3): 725-41.
[33] 罗钜, 刘辉, 高雁飞, et al. 边界层吸入式电动涵道风扇设计研究 [J]. 航空动力, 2023, 4: 39-41.
[34] MCDILL P L. An experimentalevaluationof S-duct inlet-diffuser configurations for turboprop offset gear box applicattons [R], 1986.
[35] 周慧晨, 谭慧俊, 李湘萍. 复杂变截面进气道的一种设计方法 [J]. 航空动力学报, 2009, 24(6): 1357-63.
[36] 刘雷. S弯进气道出口畸变控制及其对跨声速风扇流场影响研究 [D]. 哈尔滨; 哈尔滨工业大学, 2015.
[37] LI Z, ZHANG Y, PAN T, et al. Study on the aerodynamic performance of boundary-layer-ingesting inlet with various geometries [J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 236(1): 60-71.
[38] SAMUELSSON S. Conceptual design of propulsion systems for boundary layer ingestion [D]. Gothenburg, Sweden; Chalmers University of Technology, 2019.
[39] LEE B J, LIOU M S, KIM C. Optimizing a boundary-layer-ingestion offset inlet by discrete adjoint approach [J]. AIAA Journal, 2010, 48(9): 2008-16.
[40] KIM H, LIOU M-S. Shape design optimization of embedded engine inlets for N2B hybrid wing-body configuration [J]. Aerospace Science and Technology, 2013, 30(1): 128-49.
[41] CHIANG C, KOO D, ZINGG D W. Aerodynamic Shape Optimization of an S-Duct Intake for a Boundary Layer Ingesting Engine [Z]. Aiaa Aviation 2021 Forum. 2021.10.2514/6.2021-2468
[42] GAGNON H, ZINGG D W. Two-Level Free-Form and Axial Deformation for Exploratory Aerodynamic Shape Optimization [J]. AIAA Journal, 2015, 53(7): 2015-26.
[43] KOO D, ZINGG D W, CHISHTY W A, et al. Optimizing intakes for embedded engines [Z]. ISABE-2019. 2019
[44] CLARK C E, RASIMARZABADI F, ELLA H A E, et al. S-duct with boundary layer ingestion: Geometry optimization and validation [Z]. 2024
[45] KENWAY G K, KIRIS C C. Aerodynamic Shape Optimization of the STARC-ABL Concept for Minimal Inlet Distortion [Z]. 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2018.10.2514/6.2018-1912
[46] KUCUK U C, TUNCER I H. Adjoint Based Shape Optimization of an S-Shaped Duct with SU2 [Z]. AIAA SCITECH 2022 Forum. 2022.10.2514/6.2022-0207
[47] KAMAT V, RAO V, XU M, et al. Flow Distortion Based S-Duct Optimization using Adjoint Methodology [Z]. Aiaa Aviation 2020 Forum. 2020.10.2514/6.2020-2755
[48] 于广元. 基于自由变形技术的伴随方法 优化设计大曲率扩压通道 [D]; 南京航空航天大学, 2014.
[49] LEE B J, KIM C. Automated design methodology of turbulent internal flow using discrete adjoint formulation [J]. Aerospace Science and Technology, 2007, 11(2-3): 163-73.
[50] 唐静, 贾洪印, 李彬, et al. DSI 进气道鼓包外形优化 [J]. 西北工业大学学报, 2017, 35.
[51] 曾丽芳, 胡建新, 潘定一, et al. 亚声速无人机S弯进气道的多点多目标优化设计 [J]. 推进技术, 2021, 42(3): 495-504.
[52] 张乐, 周洲, 许晓平. 飞翼布局无人机保形非对称Ｓ弯 进气道设计及优化 [J]. 航空动力学报, 2016, 31(11): 2682-90.
[53] CHIEREGHIN N, GUGLIELMI L, SAVILL A M, et al. Shape Optimization of a Curved Duct with Free Form Deformations; proceedings of the 23rd AIAA Computational Fluid Dynamics Conference, Denver, Colorado, F, 2017 [C].
[54] ARANAKE A, LEE J G, KNIGHT D, et al. Automated Design Optimization of a Three-Dimensional Subsonic Diffuser [J]. Journal of Propulsion and Power, 2011, 27(4): 838-46.
[55] HE Y-B, YANG Q-Z, SHI Y-Q, et al. Multi-objective optimization design of S-shaped inlet with internal bump [J]. Aerospace Science and Technology, 2022, 130.
[56] RODRIGUEZ D L. Multidisciplinary Optimization Method for Designing Boundary-Layer-Ingesting Inlets [J]. Journal of Aircraft, 2009, 46(3): 883-94.
[57] RODRIGUEZ D, KROO I. A 2D multidisciplinary design method for boundary layer ingesting inlets [Z]. 37th Aerospace Sciences Meeting and Exhibit. 1999.10.2514/6.1999-838
[58] FLOREA R V, REBA R, VANSLOOTEN P R, et al. Preliminary Design for Embedded Engine Systems [Z]. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition. Orlando, Florida. 2009
[59] SEDERBERG T W, PARRY S R. Free-Form Deformation of Solid Geometric Models; proceedings of the Proceedings of the 13th annual conference on Computer graphics and interactive techniques, F, 1986 [C].
[60] FLOREA R V, VOYTOVYCH D, TILLMAN G, et al. Aerodynamic analysis of a boundary-layer-ingesting distortion-tolerant fan [Z]. Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. San Antonio, Texas, USA. 2013
[61] WOLTER J D, AREND D J, HIRT S M, et al. Development of a rotating rake array for boundary-layer-ingesting fan-stage measurements [Z]. 53rd AIAA/SAE/ASEE Joint Propulsion Conference. 2017
[62] MAGRINI A, ALLEGRETTA E, BATTISTON A, et al. Development and test of aft-fuselage BLI propulsor experiment [J]. AIAA Journal, 2025, 63(5): 1940-57.
[63] BABCOCK D A, NETO L T, DAVIS Z S. Summary of the 4thPropulsion Aerodynamics Workshop: S-duct Results [Z]. 2019
[64] DORGAN A J, WINKLER C M. BCFD analysis for the 1st AIAA propulsion workshop: S-duct results [Z]. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. 2013.10.2514/6.2013-3792
[65] BABCOCK D A, MANI M. BCFD simulations of the 2nd AIAA propulsion and aerodynamics workshop: s-duct with vortex generators [Z]. 51st AIAA/SAE/ASEE Joint Propulsion Conference. 2015.10.2514/6.2015-3959
[66] SOLORZANO FLORES H A, BONNAUD C, ATINAULT O, et al. Numerical turbulence modeling in a transonic boundary-layer ingestion intake [J]. Journal of Propulsion and Power, 2025, 41(2): 210-25.
[67] BERENS T M, DELOT A-L, TORMALM M H, et al. Numerical and experimental investigations on highly integrated subsonic air intakes [Z]. 52nd Aerospace Sciences Meeting. 2014.10.2514/6.2014-0722
[68] BERENS T M, DELOT A-L, CHEVALIER M, et al. Numerical simulations for high offset intake diffuser flows [Z]. 52nd Aerospace Sciences Meeting. 2014.10.2514/6.2014-0371
[69] THOMPSON R J, KOMIVES J R. Compressible flow through a diffusing serpentine inlet duct assessed with wall-modeled large eddy simulation [Z]. AIAA Aviation 2019 Forum. 2019.10.2514/6.2019-3702
[70] GUERRERO-HURTADO M, ZACHOS P, MACMANUS D, et al. Unsteady swirl distortion characteristics for S-ducts using Lattice Boltzmann and time-resolved, stereo PIV methods [Z]. AIAA Propulsion and Energy 2019 Forum. 2019.10.2514/6.2019-4275
[71] SANTOS F L D, EVEN N A P, BOTERO-BOLíVAR L, et al. Influence of surface roughness geometry on trailing edge wall pressure fluctuations and noise [Z]. AIAA Aviation 2021 Forum. 2021
[72] OTTEN L J, VAN KUREN J T. Artificial thickening of high subsonic mach number boundary layers [J]. AIAA Journal, 1976, 14(11): 1528-33.
[73] HARDIN L W, COUSINS W T, WOLTER J D, et al. Data analysis techniques for fan performance in highlydistorted flows from boundary layer ingesting inlets [Z]. 2018 AIAA Aerospace Sciences Meeting. 2018
[74] WANG K, HUANG H-X, LIU L, et al. A new distortion evaluation method based on geometric association for arbitrary cross-sectional shape of inlet [J]. Aerospace Science and Technology, 2022, 128.
[75] MAGHSOUDI I, VAZIRY M A, MAHMOODI M. Experimental investigation of flow and distortion mitigation by mechanical vortex generators in a coupled serpentine inlet-turbofan engine system [J]. Chinese Journal of Aeronautics, 2020, 33(5): 1375-91.
[76] WANG K, LIU L, HUANG H-X, et al. Behavior of flow distortion within a boundary layer ingestion inlet [J]. Aerospace Science and Technology, 2024, 146.
[77] MA T, LU H, LI Q. A systematic review of boundary layer ingestion (BLI) fan: Current Status and future perspectives [J]. Progress in Aerospace Sciences, 2025, 154.
[78] WELLBORN S R, REICHERT B A, OKIISHI T H. An experimental investigation of the flow in a diffusing s-duct
[Z]. 28th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, SAE, ASME, and ASEE. 1992
[79] LUCAS J R. Effect of BLI-type inlet distortion on turbofan engine performance [D]; Virginia Polytechnic Institute and State University, 2013.
[80] MIGLIORINI M, ZACHOS P K, MACMANUS D G, et al. A study on the development of the flow distortion downstream of an s-duct intake [Z]. Stockholm,sweden,4-9 september,2022. 2022
[81] M?RTENSSON H. Fan performance and aerodynamic forces with boundary layer ingestion [D]; KTH Royal Institute of Technology, 2025.
[82] GLADIN J, SANDS J, KESTNER B, et al. Effects of boundary layer ingesting (BLI) propulsion systems on engine cycle selection and HWB vehicle sizing [Z]. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2012.10.2514/6.2012-837
[83] HALL D K, GREITZER E M, TAN C S. Analysis of fan stage conceptual design attributes for boundary layer ingestion [J]. Journal of Turbomachinery, 2017, 139(7).
[84] M?RTENSSON H, RASIMARZABADI F. Effects of distortion on a BLI fan [J]. The Aeronautical Journal, 2024, 128(1325): 1362-78.
[85] REEDY T M. Analysis of radial inlet distortion on transonic fan performance [D]; Brigham Young University, 2025.
[86] MA S, WANG Z, HU J. Response and stall mechanism for axial compressor under rotating inlet distortion [J]. Physics of Fluids, 2025, 37.
[87] PEROVIC D, HALL C A, GUNN E J. Stall Inception in a boundary layer ingesting fan [J]. Journal of Turbomachinery, 2019, 141(9).
[88] ALLAN B, OWENS L, LIN J. Optimal design of passive flow control for a boundary-layer-ingesting offset inlet using design-of-experiments [Z]. 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada. 2006.10.2514/6.2006-1049
[89] KUCUK U C, BARAN ? U, UZOL O. Passive flow control in boundary layer ingesting semi submerged inlet; proceedings of the 51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, F, 2015 [C].
[90] YI J, KIM C, LEE B J. Adjoint-based design optimization of vortex generator in an s-shaped subsonic inlet [J]. AIAA Journal, 2012, 50(11): 2492-507.
[91] SCRIBBEN A R, NG W, BURDISSO R. Effectiveness of a serpentine inlet duct flow control technique at design and off-design simulated flight conditions [J]. J Turbomach, 2006, 128(2): 332-9.
[92] OWENS L R, ALLAN B G, GORTON S A. Boundary-layer-ingesting inlet flow control [J]. Journal of Aircraft, 2008, 45(4): 1431-40.
[93] ANDERSON B H, MILLER D N, ADDINGTON G A, et al. Optimal micro-jet flow control for compact air vehicle inlets [R], 2004.
[94] GISSEN A N, VUKASINOVIC B, MCMILLAN M L, et al. Distortion management in a boundary layer ingestion inlet diffuser using hybrid flow control [J]. Journal of Propulsion and Power, 2014, 30(3): 834-44.
[95] JIANG F, KONTIS K, WHITE C. Numerical investigation and mode analysis of the S-duct [J]. Physics of Fluids, 2024, 36(11).
[96] 黄河峡, 孙姝, 于航, et al. 亚声速S弯进气道研究的新进展 [J]. 推进技术, 2020, 41(12): 2641-58.
[97] 战培国, 程娅红, 赵昕. 主动流动控制技术研究 [J]. 航空科学技术, 2010, 126(05): 2-6.
[98] HARRISON E A, ANDERSON J, FLEMING J L, et al. Computational Analysis of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser [Z]. 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada. 2006
[99] FERRAR A M, O’BRIEN W F, NG W F, et al. Active control of flow in serpentine inlets for blended wing-body aircraft [Z]. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Denver, Colorado. 2009
[100] 刘雷, 陈浮, 宋彦萍, et al. 大量附面层吸入Ｓ弯进气道内吹气控制 [J]. 航空动力学报, 2015, 30(10): 2498-507.
[101] GHAEDAMINI HAROUNI A. Flow control of a boundary layer ingesting serpentine diffuser via blowing and suction [J]. Aerospace Science and Technology, 2014, 39: 472-80.
[102] GORTON S, OWENS L, JENKINS L, et al. Active Flow Control on a Boundary-Layer-Ingesting Inlet [Z]. 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada. 2004.10.2514/6.2004-1203
[103] HARRISON N A, ANDERSON J, FLEMING J L, et al. Active flow control of a boundary layer-ingesting serpentine inlet diffuser [J]. Journal of Aircraft, 2013, 50(1): 262-71.
[104] GARTNER J, AMITAY M. Flow Control in a Diffuser at Transonic Conditions [Z]. AIAA Aviation,45th AIAA Fluid Dynamics Conference. Dallas, TX. 2015.10.2514/6.2015-2484
[105] HARRISON N A, ANDERSON J, FLEMING J L, et al. Experimental Investigation of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser [Z]. 45th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada. 2007
[106] LAKEBRINK M T, MANI M. Numerical Investigation of Dynamic Distortion and Flow Control in a Serpentine Diffuser [Z]. 2018 AIAA Aerospace Sciences Meeting. 2018.10.2514/6.2018-1283
[107] 孟腾, 董金钟, 吴西云. 流体振荡器在进气道流动控制中的应用研究 [J]. 科学技术与工程, 2016, 16(32): 1671-815.
[108] VUKASINOVIC B, BURROWS T J, GLEZER A, et al. Experimental and Numerical Investigation of Controlled Flow Distortion in a Subsonic Offset Diffuser by Trapped Vorticity [Z]. 55th AIAA Aerospace Sciences Meeting. 2017.10.2514/6.2017-1454
[109] 王士奇. 流体振荡器：一种有前途的非稳态激励器 [J]. 航空动力, 2022, 1: 18-21.
[110] 陈占军, 王晋军. 合成射流改善 S 形进气道流场特性的研究 [J]. 中国科学: 技术科学, 2012, 42(9): 1054-60.
[111] 李斌斌, 程克明, 顾蕴松. 斜出口合成射流激励器Ｓ进气道分离流动控制 [J]. 实验流体力学, 2012, 26(2): 34-7.
[112] 牛中国, 杜希奇, 金沙, et al. 进气道零质量射流控制技术研究 [Z]. 第五届中国航空学会青年科技论坛. 南昌. 2012
[113] AMITAY M, PITT D, GLEZER A. Separation control in duct flows [J]. Journal of Aircraft, 2002, 39(4): 616-20.
[114] LIU R-B, MEI X-Y, XUE S-H, et al. Active flow control of S-duct by plasma synthetic jet [J]. Journal of Zhejiang University-SCIENCE A, 2022, 23(8): 652-68.
[115] GROSSMAN K, BOHDAN C, VANWIE D. Sparkjet Actuators for Flow Control [Z]. 41st Aerospace Sciences Meeting and Exhibit. 2003.10.2514/6.2003-57
[116] 周岩, 罗振兵, 王林, et al. 等离子体合成射流激励器及其流动控制 技术研究进展 [J]. 航空学报, 2022, 43(3): 025027.
[117] WANG H-Y, LI J, JIN D, et al. Response of the shock wave/boundary layer interaction to the plasma synthetic jet [J]. Acta Physica Sinica, 2017, 66(8).
[118] ZONG H, CHIATTO M, KOTSONIS M, et al. Plasma synthetic jet actuators for active flow control [J]. Actuators, 2018, 7(4).
[119] YANG H, LI F, SONG Y, et al. Numerical investigation of electrohydrodynamic (EHD) flow control in an s-shaped duct [J]. Plasma Science and Technology, 2012, 14(10): 897-904.
[120] JIANG F, KONTIS K, WHITE C. Plasma flow control inside the S-duct [J]. Physics of Plasmas, 2025, 32(3).
[121] ANDERSON B. Active "Fail Safe" Micro-Array Flow Control for Advanced Embedded Propulsion Systems [Z]. 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. 2009.10.2514/6.2009-741
[122] LIU L, CHEN F, LUO K, et al. Blowing-suction control in s-shaped inlet and its impact on fan-stage performance [J]. AIAA Journal, 2019, 57(9): 3954-68.
[123] XU K, ZHA G. System energy benefit using co-flow jet active separation control for a serpentine duct [J]. Aerospace Science and Technology, 2022, 128.
[124] BURROWS T J, VUKASINOVIC B, LAKEBRINK M T, et al. Control of Flow Distortion in Offset Diffusers Using Trapped Vorticity [J]. International Journal of Heat and Fluid Flow, 2019, 75: 122-34.
CJA