Virtual Assembly of an Airplane Turbine Engine

Author : Ali AHMAD, Abdulrahman M. AL-AHMARI,Muhammad USMAN ASLAM ,Mustufa H. ABIDI , Saber DARMOUL Department of Engineering Technology, Northwestern State University, Natchitoches, LA, USAAdvanced Manufacturing Institute, College of Engineering, King Saud University,Riyadh, Saudi ArabiaIndustrial Engineering Department, College of Engineering, King Saud University,Riyadh, Saudi Arabia Year : 2015 Doi : 10.1016/j.ifacol.2015.06.335 Keywords: Virtual reality, prototyping, […]

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An automated airplane detection system for large panchromatic image with high spatial resolution

Author : Zhenyu An,Zhenwei Shi,Xichao Teng,Xinran Yu,Wei Tang Image Processing Center, School of Astronautics, Beihang University, PR China College of Aerospace Science and Engineering, National University of Defense Technology,PR China Year : 2013 Doi : 10.1016/j.ijleo.2013.12.003 Keywords: Airplane detection ,Line segment detector (LSD) ,Circle frequency filter,Histograms of Oriented Gradients (HOG) ,AdaBoost

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Experimental research on impact loading characteristics by full-scale airplane impacting on concrete target

Author : Zhuo-ping Duan,Lian-sheng Zhang,Li-jing Wen,Chao Guo, Zhi-ling Bai, Zhuo-cheng Ou,Feng-lei Huan The State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology,ChinaDepartment of Nuclear and Radiation Safety Research, Ministry of Environmental Protection Nuclear and Radiation Safety Center, Beijing ,China Year : 2018 Doi : 10.1016/j.nucengdes.2018.01.021 Keywords: Full-scale J-6 airplane ,Impact test ,Movable […]

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Effect of pitch angle on initial stage of a transport airplane ditching

Author : Guo Baodong ,Liu Peiqing,Qu Qiulin,Wang Jiawen Institute of Fluid Mechanics, Beihang University,ChinaKey Laboratory of Fluid Mechanics, Ministry of Education, Beihang University,China Year : 2013 Doi : 10.1016/j.cja.2012.12.024 Keywords : Crashworthiness,Fluid structure interaction, Hydrodynamics ,Multiphase flow,Transport aircraft,Water landing

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Application of ICC LPV control to a blended-wing-body airplane with guaranteed H∞ performance

Author : Tianyi He,Ali K. Al-Jiboory,Guoming G. Zhu,Sean S.-M. Swei, Weihua Su Department of Mechanical Engineering, Michigan State University,USAIntelligent Systems Division, NASA Ames Research Center,USADepartment of Aerospace Engineering and Mechanics, University of Alabama,USA Year : 2018 Doi : 10.1016/j.ast.2018.07.046

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Prediction of icing effects on the lateral/directional stability and control of light airplanes

Author : Amanda Lampton , John Valasek Texas A&M University, College Station , United States Year : 2011 Doi : 10.1016/j.ast.2011.08.005 Keywords : Six degree-of-freedom simulation , Stability derivatives , Modeling of icing effects , Distributed icing , Icing severity , Sensitivity to pilot input

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Airplane detection based on rotation invariant and sparse coding in remote sensing images

Author : Liu Liu, Zhenwei Shi Image Processing Center, School of Astronautics, Beihang University, Beijing, China Year : 2014 Doi : 10.1016/j.ijleo.2014.06.062 Keywords: Airplane detection , Sparse coding ,Rotation invariant, Radial gradient transform , Constraint pooling

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Stability characteristics of the single-engine tractor propeller airplane in climb

Author : Miodrag Milenkovic-Babic´, Marija Samardžic´, Predrag Stojakovic´, Boško Rašuo Military Technical Institute, Belgrade, SerbiaFaculty of Mechanical Engineering, University of Belgrade, Serbia Year : 2015 Doi : 10.1016/j.ast.2015.07.017 Keywords: Single-engine airplane , Longitudinal stability reserve , Power effects , Neutral point

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Performances of a small hypersonic airplane (HyPlane)

Author : Raffaele Savino , Gennaro Russo , Vera D’Oriano , Michele Visone ,Manuela Battipede , Piero Gili Department of Industrial Engineering, University of Naples “Federico II”, P.le Tecchio 80, 80125 Napoli, ItalyTRANS-TECH Srl and Space Renaissance Italia, ItalyBLUE Engineering Srl, ItalyDepartment of Mechanical and Aerospace Engineering, Polytechnic of Turin, Italy Year : 2015 Doi […]

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Data mining for decision support with uncertainty on the airplane

Author : A. Senea , B. Kamsu-Foguemb , P. Rumeau Toulouse INP-ENIT, Université de Toulouse, Laboratoire Génie de Production, Ecole Nationale d’Ingénieurs de Tarbes, FranceToulouse Paul Sabatier University, Laboratoire de Gérontechnologie La Grave CHU Toulouse/Gérontopôle/UMR1027Inserm, Université de Toulouse3, Toulouse, France Year : 2018 Doi : 10.1016/j.datak.2018.06.002 Keywords: Dempster-Shafer theory , Frequent pattern mining , Semantic […]

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Single propeller airplane minimal flight speed based upon the lateral maneuver condition

Author : Predrag Stojakovic, Bosko Rasuo Military Technical Institute, Zarkovo, Belgrade, SerbiaUniversity of Belgrade, Faculty of Mechanical Engineering, Belgrade, Serbia Year : 2016 Doi : 10.1016/j.ast.2015.12.012 Keywords: Asymmetric airplane loads , Flight controls , Flight envelope , Terminal flight phases

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Rotation-and-scale-invariant airplane detection in high-resolution satellite images based on deep-Hough-forests

Author : Yongtao Yu , Haiyan Guan , Dawei Zai , Zheng Ji College of Computer Engineering, Huaiyin Institute of Technology, Huaian, JS 223003, ChinaCollege of Geography and Remote Sensing, Nanjing University of Information Science and Technology, Nanjing, JS 210044, ChinaDepartment of Computer Science, Xiamen University, Xiamen, FJ 361005, ChinaSchool of Remote Sensing Information and […]

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