A novel optimization method for maintaining aerodynamic performances in noise reduction design (English)
- New search for: Tao, J.
- New search for: Sun, G.
- New search for: Tao, J.
- New search for: Sun, G.
In:
AEROSPACE SCIENCE AND TECHNOLOGY
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43
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415-422
;
2015
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ISSN:
- Article (Journal) / Print
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Title:A novel optimization method for maintaining aerodynamic performances in noise reduction design
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Contributors:
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Published in:AEROSPACE SCIENCE AND TECHNOLOGY ; 43 ; 415-422
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Publisher:
- New search for: Elsevier Science B.V., Amsterdam.
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Publication date:2015-01-01
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Size:8 pages
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ISSN:
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Type of media:Article (Journal)
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Type of material:Print
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Language:English
- New search for: 629.105
- Further information on Dewey Decimal Classification
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Classification:
DDC: 629.105 -
Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents – Volume 43
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Three dimensional graded finite element elasticity shear buckling analysis of FGM annular sector platesAsemi, K. / Salehi, M. / Akhlaghi, M. et al. | 2015
- 14
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Pseudo steady state filters for target tracking with polar measurementsAbdelkrim, Meche / Mohammed, Dahmani / Mokhtar, Keche et al. | 2015
- 21
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Parametric and nonparametric system identification of an experimental turbojet engineTavakolpour-Saleh, A.R. / Nasib, S.A.R. / Sepasyan, A. / Hashemi, S.M. et al. | 2015
- 30
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Calibration of cross quadratic term of gyro accelerometer on centrifuge and error analysisWang, Shiming / Ren, Shunqing et al. | 2015
- 37
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Hygrothermal analysis of a rotating smart exponentially graded cylindrical shell with imperfect bonding supported by an elastic foundationSaadatfar, M. / Aghaie-Khafri, M. et al. | 2015
- 51
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Wing weight model for conceptual design of nonplanar configurationsAndrews, Stephen A. / Perez, Ruben E. / Wowk, Diane et al. | 2015
- 63
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Effects of suspension line on flow field around a supersonic parachuteXue, Xiao-peng / Koyama, Hiroto / Nakamura, Yoshiaki / Wen, Chih-Yung et al. | 2015
- 71
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PID guidance law design using short time stability approachGolestani, Mehdi / Mohammadzaman, Iman et al. | 2015
- 77
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Stochastic optimal control for aircraft conflict resolution under wind uncertaintyMatsuno, Yoshinori / Tsuchiya, Takeshi / Wei, Jian / Hwang, Inseok / Matayoshi, Naoki et al. | 2015
- 89
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Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loadingScarselli, G. / Castorini, E. / Panella, F.W. / Nobile, R. / Maffezzoli, A. et al. | 2015
- 96
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The aerodynamic design evaluation of a blended-wing-body configurationDehpanah, Payam / Nejat, Amir et al. | 2015
- 111
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A trended Kriging model with Formula Not Shown indicator and application to design optimizationKwon, H. / Choi, S. et al. | 2015
- 111
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A trended Kriging model with indicator and application to design optimizationKwon, Hyungil / Choi, Seongim et al. | 2015
- 126
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Surrogate models and mixtures of experts in aerodynamic performance prediction for aircraft mission analysisLiem, Rhea P. / Mader, Charles A. / Martins, Joaquim R.R.A. et al. | 2015
- 152
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Supercritical natural laminar flow airfoil optimization for regional aircraft wing designZhang, Yufei / Fang, Xiaoming / Chen, Haixin / Fu, Song / Duan, Zhuoyi / Zhang, Yanjun et al. | 2015
- 165
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Estimation of necessary laser power to deflect near-Earth asteroid using conceptual variable-laser-power ablationSong, Young-Joo / Park, Sang-Young et al. | 2015
- 176
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Elastoplastic buckling analysis of thin-walled structuresRuocco, Eugenio et al. | 2015
- 191
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Relative positioning of spacecraft in intense ionospheric conditions by GPSTancredi, U. / Allende-Alba, G. / Renga, A. / Montenbruck, O. / Grassi, M. et al. | 2015
- 199
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The evaluation of a detached eddy simulation based on the k–ω––f model with three flow configurationsMirzaei, M. / Sohankar, A. et al. | 2015
- 199
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The evaluation of a detached eddy simulation based on the k–ω– Formula Not Shown –f model with three flow configurationsMirzaei, M. / Sohankar, A. et al. | 2015
- 213
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Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensationWu, Shunan / Wang, Rui / Radice, Gianmarco / Wu, Zhigang et al. | 2015
- 219
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Radially accelerated trajectories for variable mass spacecraftQuarta, Alessandro A. / Mengali, Giovanni et al. | 2015
- 226
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RBF neural network based second-order sliding mode guidance for Mars entry under uncertaintiesLi, Shuang / Jiang, Xiuqiang et al. | 2015
- 236
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Modeling and analysis of dynamics for spacecraft relative motion actuated by inter-satellite non-contacting forceZhang, Yuan-wen / Yang, Le-ping / Zhu, Yan-wei / Huang, Huan / Cai, Wei-wei et al. | 2015
- 245
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Aerodynamic optimisation of a camber morphing aerofoilFincham, J.H.S. / Friswell, M.I. et al. | 2015
- 256
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Comparison between synthetic jets and continuous jets for active flow control: Application on a NACA 0015 and a compressor stator cascadeDe Giorgi, M.G. / De Luca, C.G. / Ficarella, A. / Marra, F. et al. | 2015
- 281
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Active aeroelastic control with time delay for targeted flutter modesSingh, Kumar Vikram et al. | 2015
- 289
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An active–passive acoustics approach for bond-line condition monitoring in aerospace skin stiffener panelsVanniamparambil, Prashanth Abraham / Carmi, Rami / Khan, Fuad / Cuadra, Jefferson / Bartoli, Ivan / Kontsos, Antonios et al. | 2015
- 301
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Towards analysis and predicting maps of ultraviolet index from experimental astronomical parameters (solar elevation, total ozone level, aerosol index, reflectivity). Artificial neural networks global scale approachLatosińska, Jolanta Natalia / Latosińska, Magdalena / Bielak, Jarosław et al. | 2015
- 314
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Fabrication of a thermoplastic matrix composite stiffened panel by induction weldingPappadà, Silvio / Salomi, Andrea / Montanaro, Jeanette / Passaro, Alessandra / Caruso, Antonio / Maffezzoli, Alfonso et al. | 2015
- 321
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Maneuver characteristics analysis for hypersonic glide vehiclesLi, Guanghua / Zhang, Hongbo / Tang, Guojian et al. | 2015
- 329
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Robust optimal sliding mode control for spacecraft position and attitude maneuversPukdeboon, Chutiphon / Kumam, Poom et al. | 2015
- 343
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Interaction of microwave and laser discharge resulting “heat spots” with supersonic combined cylinder bodiesAzarova, O.A. / Knight, D.D. et al. | 2015
- 350
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Dimensioning of automated regenerative cooling: Setting of high-end experimentTaddeo, L. / Gascoin, N. / Fedioun, I. / Chetehouna, K. / Lamoot, L. / Fau, G. et al. | 2015
- 360
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Numerical analysis of hypersonic flows around blunt-nosed models and a space vehicleSaldivar Massimi, Heriberto / Shen, Hua / Wen, Chih-Yung / Chen, Yen-Sen / Liang, Shen-Min et al. | 2015
- 372
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Drag-tracking guidance for entry vehicles without drag rate measurementYan, Han / He, Yingzi et al. | 2015
- 381
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Fractional order adaptive fuzzy sliding mode controller for a position servo system subjected to aerodynamic loading and nonlinearitiesUllah, Nasim / Shaoping, Wang / Khattak, Muhammad Irfan / Shafi, Muhammad et al. | 2015
- 388
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Combustion noise characteristics of an experimental 2D trapped vortex combustorEzhil Kumar, P.K. / Mishra, D.P. et al. | 2015
- 395
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An experimental study on the interaction between free-stream turbulence and a wing-tip vortex in the near-fieldAhmadi-Baloutaki, Mojtaba / Carriveau, Rupp / Ting, David S.-K. et al. | 2015
- 406
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Dynamic stall control optimization of rotor airfoil via variable droop leading-edgeZhao, Guo-qing / Zhao, Qi-jun et al. | 2015
- 415
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A novel optimization method for maintaining aerodynamic performances in noise reduction designTao, Jun / Sun, Gang et al. | 2015
- 423
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DDES study of the aerodynamic forces and flow physics of a delta wing in static ground effectQin, Yunpeng / Qu, Qiulin / Liu, Peiqing / Tian, Yun / Lu, Zhe et al. | 2015
- 437
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Challenges in the development of a slow burning solid rocket boosterParhi, Achutananda / Mahesh, V. / Shaji, A. / Levin, G. / Abraham, P.J. / Srinivasan, V. et al. | 2015
- 445
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Experimental research on rotating detonation in liquid fuel–gaseous air mixturesKindracki, Jan et al. | 2015
- 454
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A new approach to autonomous rendezvous for spacecraft with limited impulsive thrust: Based on switching control strategyYang, Xuebo / Cao, Xibin et al. | 2015
- 463
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Evaluating the longitudinal stability of an UAV using a CFD-6DOF modelSandoval, Pablo / Cornejo, Pablo / Tinapp, Frank et al. | 2015
- 471
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Experimental study of the effect of blade curvature and aspect ratio on the performance of a rotary-wing deceleratorMartiarena, Juan Francisco / Nadal Mora, Vicente / Piechocki, Joaquín et al. | 2015
- IFC
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Editorial Board| 2015