Surrogate-Based Aerodynamic Shape Optimization by Variable-Resolution Models (English)
- New search for: Koziel, Slawomir
- New search for: Leifsson, Leifur
- New search for: Koziel, Slawomir
- New search for: Leifsson, Leifur
In:
AIAA Journal
;
51
, 1
;
94-106
;
2012
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ISSN:
- Article (Journal) / Electronic Resource
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Title:Surrogate-Based Aerodynamic Shape Optimization by Variable-Resolution Models
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Contributors:Koziel, Slawomir ( author ) / Leifsson, Leifur ( author )
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Published in:AIAA Journal ; 51, 1 ; 94-106
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Publisher:
- New search for: The American Institute of Aeronautics and Astronautics
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Publication date:2012-11-22
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Size:13 pages
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ISSN:
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DOI:
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Type of media:Article (Journal)
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Type of material:Electronic Resource
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Language:English
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Keywords:
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Source:
Table of contents – Volume 51, Issue 1
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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Announcements, Comments, and Acknowledgments| 2013
- 13
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Reviewers for 1 October 2011–30 September 2012| 2013
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Editorial Policy Statement on Numerical and Experimental Accuracy| 2013
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Ethical Standards for Publication of Aeronautics and Astronautics Research| 2013
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AIAA Manuscript Review Process| 2013
- 20
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Transient Loads Control of a Variable Speed Rotor During Lagwise Resonance CrossingHan, D et al. | 2013
- 20
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Transient Loads Control of a Variable Speed Rotor During Lagwise Resonance CrossingHan, Dong / Wang, Joseph / Smith, Edward C. / Lesieutre, George A. et al. | 2012
- 30
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Hybrid Immersed Boundary Method for Airfoils with a Trailing-Edge FlapZhu, Wei Jun / Behrens, Tim / Shen, Wen Zhong / Sørensen, Jens Nørkær et al. | 2012
- 30
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FLUID DYNAMICS - Hybrid Immersed Boundary Method for Airfoils with a Trailing-Edge FlapZhu, W J et al. | 2013
- 42
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PROPULSION AND POWER - Analytical and Numerical Study of Combustion Noise Through a Subsonic NozzleDurán, I et al. | 2013
- 42
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Analytical and Numerical Study of Combustion Noise Through a Subsonic NozzleDurán, Ignacio / Moreau, Stéphane / Poinsot, Thierry et al. | 2012
- 53
-
Adaptive Cartesian Immersed Boundary Method for Simulation of Flow over Flexible GeometriesHarris, Robert E. et al. | 2012
- 70
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Mean Streamwise Centerline Velocity Decay and Entrainment in Triangular and Circular JetsQuinn, W. R. / Azad, M. / Groulx, D. et al. | 2012
- 80
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Two-Dimensional Shock-Wave/Boundary-Layer Interaction in the Presence of Entropy LayerBorovoy, Volf Y. / Egorov, Ivan V. / Skuratov, Arkady S. / Struminskaya, Irina V. et al. | 2012
- 94
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Surrogate-Based Aerodynamic Shape Optimization by Variable-Resolution ModelsKoziel, Slawomir / Leifsson, Leifur et al. | 2012
- 107
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Investigation of Flows Around a Rudimentary Landing Gear with Advanced Detached-Eddy-Simulation ApproachesXiao, Zhixiang / Liu, Jian / Luo, Kunyu / Huang, Jingbo / Fu, Song et al. | 2012
- 126
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Derivative-Enhanced Variable Fidelity Surrogate Modeling for Aerodynamic FunctionsYamazaki, Wataru / Mavriplis, Dimitri J. et al. | 2012
- 138
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STRUCTURAL MECHANICS AND MATERIALS - Hybrid Dimension-Reduction Method for Robust Design OptimizationLi, H-S et al. | 2013
- 138
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Hybrid Dimension-Reduction Method for Robust Design OptimizationLi, Hong-Shuang / Ma, Chao et al. | 2012
- 145
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Effect of Stroke Deviation on Forward Flapping FlightViswanath, Kamal / Tafti, Danesh K. et al. | 2012
- 161
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Postcritical Analysis of PrandtlPlane Joined-Wing ConfigurationsDemasi, Luciano / Cavallaro, Rauno / Márquez Razón, Alan et al. | 2012
- 178
-
Real-Time Estimation of Time-Varying Bending Modes Using Fiber Bragg Grating Sensor Arrays| 2012
- 178
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Real-Time Estimation of Time-Varying Bending Modes Using Fiber Braqg Gratingn Sensor ArraysJiang, H et al. | 2013
- 186
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Validation of an Improved Experimental Method for Use in Impedance EductionJones, M. G. / Watson, W. R. et al. | 2012
- 186
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Validation of an Improved Experimental Method for Use in Impedance EducationJones, M.G. / Watson, W.R. et al. | 2013
- 200
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Development of a Particle–Particle Hybrid Scheme to Simulate Multiscale Transitional FlowsKumar, Rakesh / Titov, E. V. / Levin, D. A. et al. | 2012
- 218
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Lower-Bound Analysis of Fiber-Reinforced Polymeric Laminated Cylindrical ShellsWang, Hongtao / Croll, James G. A. et al. | 2012
- 226
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Effects of Oxygen Enrichment on Scramjet PerformancePetty, David J. / Wheatley, Vincent / Smart, Michael K. / Razzaqi, Sarah A. et al. | 2012
- 236
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Simultaneous Iterative Method for Eigenpair Derivatives of Damped SystemsXie, Huiqing et al. | 2012
- 240
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Vortical Interactions Behind Deployable Vortex Generator for Airfoil Static Stall ControlJoubert, G. / Le Pape, A. / Heine, B. / Huberson, S. et al. | 2012
- 253
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Feedback Mechanism in Supersonic Laminar Cavity Flows (TN)Li, W et al. | 2013
- 253
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Feedback Mechanism in Supersonic Laminar Cavity FlowsLi, Weipeng / Nonomura, Taku / Oyama, Akira / Fujii, Kozo et al. | 2012
- 257
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Master Formula for Geometrically Nonlinear Dynamic Instability of Shear Flexible BeamsRatnam, B. Subba / Rao, G. Venkateswara / Janardhana, G. Ranga et al. | 2012
- 257
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Master Formula for Geometrically Nonlinear Dynamic Instability of Shear Flexible Beams (TN)Ratnam, B S et al. | 2013
- 262
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Forced Vibration of Turbine Cascade Predicted by Transformation Techniques Considering Flow Compressibility (TN)Lee, I et al. | 2013
- 262
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Forced Vibration of Turbine Cascade Predicted by Transformation Techniques Considering Flow CompressibilityLee, Il / Shin, SangJoon / Kim, Taehyoun et al. | 2012
- 266
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Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height RoughnessDuan, Le / Wang, Xiaowen / Zhong, Xiaolin et al. | 2012
- 266
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Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness (TN)Duan, L et al. | 2013
- 270
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Abort Separation of Launch Escape System Using Aerodynamic InterferenceWang, Yunpeng / Ozawa, Hiroshi / Koyama, Hiroto / Nakamura, Yoshiaki et al. | 2012
- 270
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Abort Separation of Launch Escape System Using Aerodynamic Interference (TN)Wang, Y. / Ozawa, H. / Koyama, H. / Nakamura, Y. et al. | 2013
- 270
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LAUNCH VEHICLE AND MISSILE (LV/M) TECHNOLOGY - Abort Separation of Launch Escape System Using Aerodynamic Interference (TN)Wang, Y et al. | 2013
- 277
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Comparison of Node-Centered and Cell-Centered Unstructured Finite-Volume Discretizations: Inviscid FluxesDiskin, Boris / Thomas, James L. et al. | 2012
- 277
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ERRATUM - Comparison of Node-Centered and Cell-Centered Unstructured Finite-Volume Discretizations: Inviscid FluxesDiskin, B et al. | 2013
- 278
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Lattice Boltzmann Method: Fundamentals and Engineering Applications with Computer CodesGirimaji, Sharath et al. | 2012
- 278
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BOOK REVIEW - Lattice Boltzmann Method: Fundamentals and Engineering Applications with Computer CodesGirimaji, S et al. | 2013
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TABLES OF CONTENTS OF NON-U.S. JOURNALS - Journal of the Japan Society for Aeronautical and Space Sciences| 2013