標題: Titlebook: Advances in Multidisciplinary Analysis and Optimization; Proceedings of the 2 Raviprakash R. Salagame,Palaniappan Ramu,Dhish Kum Conference [打印本頁] 作者: 葉子 時間: 2025-3-21 19:21
書目名稱Advances in Multidisciplinary Analysis and Optimization影響因子(影響力)
書目名稱Advances in Multidisciplinary Analysis and Optimization影響因子(影響力)學科排名
書目名稱Advances in Multidisciplinary Analysis and Optimization網絡公開度
書目名稱Advances in Multidisciplinary Analysis and Optimization網絡公開度學科排名
書目名稱Advances in Multidisciplinary Analysis and Optimization被引頻次
書目名稱Advances in Multidisciplinary Analysis and Optimization被引頻次學科排名
書目名稱Advances in Multidisciplinary Analysis and Optimization年度引用
書目名稱Advances in Multidisciplinary Analysis and Optimization年度引用學科排名
書目名稱Advances in Multidisciplinary Analysis and Optimization讀者反饋
書目名稱Advances in Multidisciplinary Analysis and Optimization讀者反饋學科排名
作者: tympanometry 時間: 2025-3-21 22:42 作者: DEVIL 時間: 2025-3-22 02:52
Multi-disciplinary Analysis of a Reentry Vehicleith (1) a DC motor and (2) a brake in terms of robot safety and performance. Experimental comparisons show that the hybrid actuation with PAMs and a brake provides higher energy efficiency for control bandwidths under 2 Hz, and is capable of effectively reducing large impacts due to the brake’s high作者: 油膏 時間: 2025-3-22 05:16
Optimization of Multiple Gravity Assist Trajectories with Deep Space Maneuver Using Evolutionary Algur solutions to these challenges. Firstly, we summarize the design of our micro air vehicle, focusing on the navigation and sensing payload. Secondly, we describe the vision and state estimation algorithms used to track ground features through a sequence of images from the MAV, including stationary 作者: apropos 時間: 2025-3-22 11:37 作者: In-Situ 時間: 2025-3-22 13:34 作者: 畢業(yè)典禮 時間: 2025-3-22 20:53
Study of Wing Flutter at Preliminary Stages of Designts. This work focuses on providing a robust and versatile hybrid platform that improves payload capacity, operation time, endurance, and versatility. The Bi-modal Aerial and Terrestrial hybrid vehicle (BAXTER) is a solution that provides two modes of operation, aerial and terrestrial. BAXTER employs作者: diathermy 時間: 2025-3-23 00:12
Coupled Aero-structural Simulation Techniques Using High-Fidelity Analysis and Design Tools haptic forces (0.5–2N; square or 0.1–65Hz sine waveforms) while maintaining negligible temporal noise in pre-motor, motor, somatosensory, and visual cortex (<1?% of signal). Our results show that Haptic fMRI is a robust and reliable technique for characterizing the human brain’s motor controller.作者: 不溶解 時間: 2025-3-23 05:14 作者: intoxicate 時間: 2025-3-23 05:50 作者: Boycott 時間: 2025-3-23 10:19 作者: 進取心 時間: 2025-3-23 14:15
Performance Comparison of Discrete Kalman Filter and Dynamic Programming Technique for Pavement Rougct) such that it is ., i.e., it is view invariant and it does not require a calibrated camera. The central issue of any image-based servoing method is the estimation of the image Jacobian. This Jacobian relates the 3-D velocity field of a moving object to the image velocity field. In the past, the e作者: 整潔 時間: 2025-3-23 21:45 作者: 記憶法 時間: 2025-3-24 01:00 作者: CLAM 時間: 2025-3-24 03:02 作者: BIPED 時間: 2025-3-24 10:01 作者: 考得 時間: 2025-3-24 11:53 作者: diabetes 時間: 2025-3-24 17:53 作者: 六個才偏離 時間: 2025-3-24 21:45 作者: 樂意 時間: 2025-3-24 23:31 作者: follicular-unit 時間: 2025-3-25 06:00
Whiteness and the Future of Race Relations,locity at departure planet, the time instant at which each DSM takes place, the pericenter radius at each body and the turning angle of each hyperbola are considered for the objective function assessment. This paper evaluates some benchmark MGA mission problems with one DSM. The data of these proble作者: intention 時間: 2025-3-25 08:47 作者: AWE 時間: 2025-3-25 13:12 作者: mettlesome 時間: 2025-3-25 18:10 作者: 冒煙 時間: 2025-3-25 22:11 作者: esculent 時間: 2025-3-26 00:59
H. W. Strobel,D. K. Hammond,T. B. White constructed and CFD simulations were carried out. CFD studies were carried out to evaluate the aerodynamics of these configurations. Validation studies were done for a particular configuration at various Mach numbers. An open-source mesh generation software, Gmsh, was used along with the open-sourc作者: 蘆筍 時間: 2025-3-26 07:34 作者: Sinus-Rhythm 時間: 2025-3-26 10:33 作者: SHRIK 時間: 2025-3-26 14:35 作者: Affable 時間: 2025-3-26 20:41
https://doi.org/10.1385/1592590845tion (RBDO)—designs which would meet the required reliability in performance when the input variables undergo random variations. This piece of work combines the machine learning methods used to predict performance along with reliability analysis tools to develop a RBDO framework which can predict re作者: calamity 時間: 2025-3-26 22:25
Screening with Occult Blood Testingchassis where thickness of the selected parts forms the design variables. It is a classic MDO problem where mass is minimized while maintaining performance requirements derived from different disciplines such as durability, stiffness, NVH, and safety. Altair MDOD utilizes Altair HyperStudy. in the b作者: amygdala 時間: 2025-3-27 02:24 作者: LAVE 時間: 2025-3-27 05:48
Conference proceedings 2020opments at the core of optimization methods and its application in multiple applications. The papers showcase fundamental problems and applications which include domains such as aerospace, automotive and industrial sectors. The variety of topics and diversity of insights presented in the general fie作者: cyanosis 時間: 2025-3-27 13:12
Conference proceedings 2020ich include domains such as aerospace, automotive and industrial sectors. The variety of topics and diversity of insights presented in the general field of optimization and its use in design for different applications will be of interest to researchers in academia or industry.作者: 非秘密 時間: 2025-3-27 15:50 作者: BAIL 時間: 2025-3-27 21:39 作者: 戰(zhàn)勝 時間: 2025-3-28 00:38
H. W. Strobel,D. K. Hammond,T. B. Whitearameterizing six design variables. Some selected vortex flap geometries were then tested in a wind tunnel, and the results indicate that the approach speed target is met within all identified constraints. It is now planned to flight test the preferred shape for confirming the practical application of this concept on future naval aircraft designs.作者: 狂熱語言 時間: 2025-3-28 04:37 作者: 南極 時間: 2025-3-28 09:44 作者: 哎呦 時間: 2025-3-28 10:50 作者: Feature 時間: 2025-3-28 18:28
Lecture Notes in Mechanical Engineeringhttp://image.papertrans.cn/a/image/148996.jpg作者: Isometric 時間: 2025-3-28 19:07 作者: 一大塊 時間: 2025-3-29 00:21
978-981-15-5434-6Springer Nature Singapore Pte Ltd. 2020作者: gnarled 時間: 2025-3-29 04:28 作者: 彩色的蠟筆 時間: 2025-3-29 07:39 作者: 寒冷 時間: 2025-3-29 14:27 作者: 一美元 時間: 2025-3-29 17:24 作者: COUCH 時間: 2025-3-29 22:23 作者: 一罵死割除 時間: 2025-3-30 01:30
Katja Dahlgaard,Jesper Thorvald Troelsene energy coming to structure causes the wing to deflect and in turn the deflection is in such way that it adds energy back to the structure. The positive coupling between wing deflection and aerodynamic forces enables self-sustained oscillation, which is generally referred as flutter, and it can cau作者: 事情 時間: 2025-3-30 07:01
Martine Chevillard-Briet,Fabrice Escaffitwith the need for high-fidelity fluid and structural solvers, this multi-physics problem also requires a tight coupling strategy between the solvers and a robust methodology to handle the deformation of the CFD mesh. For partitioned solvers, it is also crucial that the coupling methodology caters fo作者: Tailor 時間: 2025-3-30 09:51
H. W. Strobel,D. K. Hammond,T. B. Whiteuld be able to accommodate the required payload volume inside it, it should have desirable aerodynamic features like low drag, low transonic shock strength, low base bending moment, etc. The PLF shape design problem is posed as a multiobjective optimization problem with minimization of drag coeffici作者: flammable 時間: 2025-3-30 12:49
H. W. Strobel,D. K. Hammond,T. B. Whitesupersonic capabilities. A sharp leading edge surface called LEVCON that can be deflected upwards for reducing approach speed has been implemented on an indigenous naval aircraft. Another solution explored in this paper is to vertically extend a panel near the wing apex called vortex flap to achieve作者: Forehead-Lift 時間: 2025-3-30 19:51
H. W. Strobel,D. K. Hammond,T. B. Whitesent paper deals with pavement roughness identification based on the dynamic response of a quarter car vehicle model. The forward problem involves computing the vehicle responses using Newmark’s beta method. Noise in the measured data poses a serious challenge to the roughness identification problem作者: investigate 時間: 2025-3-30 23:46 作者: delusion 時間: 2025-3-31 01:17
,Mutation Detection inTGF-β Receptors,nterior brackets are a prime example with a requirement of being soft to minimize head injury during impact, adequate stiffness during operation, and non-failure during abusive loadings. The problem is further compounded with the safety loadcase being a non-linear dynamic loadcase, whereas stiffness作者: lipoatrophy 時間: 2025-3-31 08:15
https://doi.org/10.1385/1592590845beams are typically designed with multiple tailor rolled blanks (TRB) to minimize mass. This poses challenge to the designer to optimize the section sizes as well as thicknesses of different regions while meeting various performance requirements. One such requirement for the door beam is not to unde作者: 飛行員 時間: 2025-3-31 11:07
Screening with Occult Blood Testingloration of design requirements of different disciplines. The MDO methodology can be adopted for design development in aerospace, automobile, and electronics domains. Altair Multidisciplinary Design Optimization Director? (MDOD) is the unique framework developed to aid rapid set-up, execution, postp作者: LASH 時間: 2025-3-31 15:53 作者: 翅膀拍動 時間: 2025-3-31 20:45
Colonoscopy as a Screening Procedure? the key contributors for thermal stresses induced in any component which in turn affects its life. Hence, design optimization studies are performed to reduce thermal gradients, especially for the components operating at high temperatures. Multi-disciplinary optimization (MDO) is performed using ISI作者: Canyon 時間: 2025-3-31 21:40
