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    Experimental investigation of isolated inlets for high agile missiles

    Herrmann, Dirk / Triesch, Klaus | Elsevier | 2006
    Keywords: Axially symmetric inlet

    Operation pattern classification of hypersonic inlets

    Chang, Juntao / Yu, Daren / Bao, Wen et al. | Elsevier | 2009
    Keywords: Hypersonic inlet

    Effects of wall cooling on performance parameters of hypersonic inlets

    Chang, Juntao / Bao, Wen / Yu, Daren et al. | Elsevier | 2009
    Keywords: Hypersonic inlet

    Switching control of thrust regulation and inlet buzz protection for ducted rocket

    Bao, Wen / Li, Bin / Chang, Juntao et al. | Elsevier | 2010
    Keywords: Inlet buzz

    Mathematical modeling and rapid recognition of hypersonic inlet buzz

    Chang, Juntao / Yu, Daren / Bao, Wen et al. | Elsevier | 2011
    Keywords: Hypersonic inlet , Inlet buzz

    Classifier utility modeling and analysis of hypersonic inlet start/unstart considering training data costs

    Chang, Juntao / Hu, Qinghua / Yu, Daren et al. | Elsevier | 2011
    Keywords: Hypersonic inlet

    A difference-fractional FOM decision method for down-selection of hypersonic compression system configurations

    Sarosh, Ali / Shi-Ming, Chen / Yun-Feng, Dong | Elsevier | 2012
    Keywords: Highly-integrated forebody–inlet configurations

    Backpressure unstart detection for a scramjet inlet based on information fusion

    Chang, Juntao / Zheng, Risheng / Wang, Lei et al. | Elsevier | 2013
    Keywords: Hypersonic inlet

    Shape design optimization of embedded engine inlets for N2B hybrid wing-body configuration

    Kim, Hyoungjin / Liou, Meng-Sing | Elsevier | 2013
    Keywords: Inlet distortion

    Numerical investigation on hydrogen combustion in a scramjet with 3D sidewall compression inlet

    Jin, Liang / Lei, Jing / Huang, Wei et al. | Elsevier | 2014
    Keywords: Inlet distortion , Sidewall compression inlet

    Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy

    Cao, Ruifeng / Chang, Juntao / Tang, Jingfeng et al. | Elsevier | 2014
    Keywords: Inlet unstart

    Design and cold flow test of a scramjet nozzle with nonuniform inflow

    Mo, Jianwei / Xu, Jinglei / Quan, Zhibin et al. | Elsevier | 2014
    Keywords: Non-uniform inlet

    Three dimensional investigation of the shock train structure in a convergent–divergent nozzle

    Mousavi, Seyed Mahmood / Roohi, Ehsan | Elsevier | 2014
    Keywords: Inlet flow total temperature

    Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance

    Teng, Jian / Yuan, Huacheng | Elsevier | 2015
    Keywords: Hypersonic inlet , Variable geometry inlet , Inlet start

    Switching control of thrust regulation and inlet unstart protection for scramjet engine based on strategy of integral initial values resetting

    Cao, Ruifeng / Chang, Juntao / Tang, Jingfeng et al. | Elsevier | 2015
    Keywords: Inlet unstart

    Novel inlet–airframe integration methodology for hypersonic waverider vehicles

    Ding, Feng / Liu, Jun / Shen, Chi-bing et al. | Elsevier | 2015
    Keywords: Inlet–airframe integration

    A new integration method based on the coupling of mutistage osculating cones waverider and Busemann inlet for hypersonic airbreathing vehicles

    Wang, Xu-dong / Wang, Jiang-feng / Lyu, Zhen-jun | Elsevier | 2016
    Keywords: Busemann inlet

    Investigation of boundary-layer ejecting for resistance to back pressure in an isolator

    He, Yubao / Huang, Hongyan / Yu, Daren | Elsevier | 2016
    Keywords: Inlet unstart

    Potential improvement of aerodynamic performance by morphing the nacelle inlet

    Majić, Frane / Efraimsson, Gunilla / O'Reilly, Ciarán J. | Elsevier | 2016
    Keywords: Nacelle inlet

    Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel

    Jiao, Xiaoliang / Chang, Juntao / Wang, Zhongqi et al. | Elsevier | 2016
    Keywords: Hypersonic inlet

    Construction methodology for lip surface of a submerged inlet

    Wang, Yuan-guang / Wang, Chang-hui / Xiao, Ying-chao et al. | Elsevier | 2016
    Keywords: Submerged inlet

    Numerical study on dynamic characteristics for sharp opening procedure of boundary-layer suction slot

    He, Yubao / Yin, Hang / Huang, Hongyan et al. | Elsevier | 2017
    Keywords: Inlet unstart , Hypersonic inlet

    Exchange inlet optimization by genetic algorithm for improved RBCC performance

    Chorkawy, G. / Etele, J. | Elsevier | 2017
    Keywords: Inlet

    Effects of injection nozzle exit width on rotating detonation engine

    Sun, Jian / Zhou, Jin / Liu, Shijie et al. | Elsevier | 2017
    Keywords: Chamber inlet state

    Computational fluid dynamics analysis of a synthesis gas turbulent combustion in a round jet burner

    Mansourian, Mohammad / Kamali, Reza | Elsevier | 2017
    Keywords: Inlet velocity

    Numerical investigation of switching mechanism for the supersonic jet element

    Xu, Y. / Zhang, G.Q. | Elsevier | 2017
    Keywords: point from main jet inlet (−0.0062,0.042) , point from main jet inlet (0.0062,0.042)

    3D inverse method of characteristics for hypersonic bump-inlet integration

    Yu, Zonghan / Huang, Guoping / Xia, Chen | Elsevier | 2019
    Keywords: Waverider-inlet integration , Hypersonic inlet

    Experimental and numerical study on the local unstart mechanism of hypersonic inlet

    Liu, Junbing / Fan, Xiaoqiang / Tao, Yuan et al. | Elsevier | 2019
    Keywords: Hypersonic inlet

    Parameterization and optimization design of a hypersonic inward turning inlet

    Xiong, Bing / Fan, Xiao-qiang / Wang, Yi | Elsevier | 2019
    Keywords: Inward turning inlet

    Effect of tangential swirl air inlet angle on the combustion efficiency of a hybrid powder-solid ramjet

    Xu, Yihua / Jia, Rui / Medina, Humberto et al. | Elsevier | 2019
    Keywords: Tangential air inlet angle

    Novel design methodology of integrated waverider with drip-like intake based on planform leading-edge definition method

    Chen, Shao-Hua / Liu, Jun / Ding, Feng et al. | Elsevier | 2019
    Keywords: Forebody-inlet and airframe axisymmetric basic flow model

    Research and development on inlets for rocket based combined cycle engines

    Shi, Lei / Yang, Yiyan / Zhao, Guojun et al. | Elsevier | 2020
    Keywords: Inlet

    A novel approach for inverse design of three-dimensional shock waves under non-uniform flows

    Zhou, Hang / Jin, Zhiguang | Elsevier | 2020
    Keywords: Integration design of waverider forebody and inlet

    Response of shock train to fluctuating angle of attack in a scramjet inlet-isolator

    Li, Nan | Elsevier | 2021
    Keywords: Hypersonic inlet-isolator

    RBF-POD reduced-order modeling of flow field in the curved shock compression inlet

    Sun, Fei / Su, Wei-Yi / Wang, Mou-Yuan et al. | Elsevier | 2021
    Keywords: Ramjet inlet

    Boundary-layer viscous correction method for hypersonic forebody/inlet integration

    Ding, Feng / Liu, Jun / Huang, Wei et al. | Elsevier | 2021
    Keywords: Forebody/inlet integration

    Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet

    Dai, Chunliang / Sun, Bo / Zhou, Shengbing et al. | Elsevier | 2022
    Keywords: Mach 12 scramjet inlet , Inlet performance

    Inlet buzz phenomenon driven by flow choking in high-enthalpy Mach 4.5 flows using circular scramjet models

    Liu, Qili / Kang, Kyungrae / Do, Hyungrok | Elsevier | 2022
    Keywords: Inlet buzz

    Suppression of flow response hysteresis in the throttling/unthrottling process for supersonic inlet

    Jin, Yi / Zhang, Yue / Li, Xin et al. | Elsevier | 2022
    Keywords: Supersonic inlet

    Non-intrusive flow diagnostics for unsteady inlet flow distortion measurements in novel aircraft architectures

    Doll, Ulrich / Migliorini, Matteo / Baikie, Joni et al. | Elsevier | 2022
    Keywords: Inlet flow distortion

    Combustion enhancement subjected to the inlet distortion in a cavity-based supersonic combustor

    Li, Jianbin / Liang, Jianhan / Sun, Mingbo et al. | Elsevier | 2023
    Keywords: Inlet distortion

    Mode identification and decomposition analysis of self-excited thermodynamic oscillations in hypersonic inlet/isolator of a scramjet

    Dai, Chunliang / Sun, Bo / Zhao, Dan et al. | Elsevier | 2023
    Keywords: Hypersonic inlet/isolator

    Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp

    Chen, Liang / Zhang, Yue / Xue, Hong-chao et al. | Elsevier | 2023
    Keywords: Inward turning inlet

    Efficient numerical prediction of blade forced response under inlet distortion

    Fang, Mingchang / Wang, Yanrong | Elsevier | 2023
    Keywords: Inlet distortion

    Partial tip air injection to extend the stall margin in an axial flow compressor with circumferential inlet distortion

    Li, Jichao / Liu, Yang / Liu, Jingyuan et al. | Elsevier | 2023
    Keywords: Circumferential inlet distortion

    Comparison of the unstart/restart processes of a two-dimensional twin-duct supersonic inlet induced by the plug throttling and thermal choking at the sideslip state

    Li, Teng-fei / Ding, Run-han / Wang, Wei-xing et al. | Elsevier | 2023
    Keywords: Two-dimensional twin-duct inlet configuration

    Aerodynamic analysis of an airframe-inlet integrated full-waverider vehicle designed by osculating cone theory

    Luo, Shibin / Tian, Jiaqi / Wang, Dou et al. | Elsevier | 2023
    Keywords: Airframe/inlet integration

    Aerodynamics and bird ingestion characteristics of a bulge-adjustable turboprop engine inlet

    Zheng, Gaojie / Tan, Huijun / Wu, Zhenlong et al. | Elsevier | 2023
    Keywords: Inlet design

    A review of the shock-dominated flow in a hypersonic inlet/isolator

    Huang, He-xia / Tan, Hui-jun / Li, Fang-bo et al. | Elsevier | 2023
    Keywords: Inlet unstart/restart

    Preventing inlet unstart in air-breathing hypersonic vehicles using adaptive backstepping control with state constraints

    Wang, Fan / Fan, Pengfei / Zhang, Jin et al. | Elsevier | 2023
    Keywords: Inlet unstart

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