標(biāo)題: Titlebook: 2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings; Volume I Song Fu Conference proceedings 2024 T [打印本頁(yè)] 作者: ODDS 時(shí)間: 2025-3-21 17:15
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings影響因子(影響力)
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings影響因子(影響力)學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings網(wǎng)絡(luò)公開度
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings被引頻次
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings被引頻次學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings年度引用
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings年度引用學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings讀者反饋
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings讀者反饋學(xué)科排名
作者: LEERY 時(shí)間: 2025-3-21 21:01
Lecture Notes in Electrical Engineeringhttp://image.papertrans.cn/012/image/100484.jpg作者: Buttress 時(shí)間: 2025-3-22 00:34
https://doi.org/10.1007/978-981-97-3998-1Asia-Pacific Technical Platform; Structures and Materials; Aerospace Academic Exchanges; Dynamics/Contr作者: 有權(quán)威 時(shí)間: 2025-3-22 05:37
978-981-97-4000-0The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor作者: 有權(quán) 時(shí)間: 2025-3-22 10:58
2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings978-981-97-3998-1Series ISSN 1876-1100 Series E-ISSN 1876-1119 作者: 退潮 時(shí)間: 2025-3-22 16:45 作者: conquer 時(shí)間: 2025-3-22 18:31 作者: MAOIS 時(shí)間: 2025-3-22 23:51
Alexandra Boldyreva,Marc Fischlind by high adaptive gain in the lateral nonlinear control of UAV in the case of traditional adaptive control method, a lateral control method of UAV Based on L1 adaptive unmatched nonlinear is proposed in this paper. Firstly, taking a scaled down UAV in the laboratory as the prototype, the lateral dy作者: Dorsal 時(shí)間: 2025-3-23 03:24
Advances in Cryptology – ASIACRYPT 2007s (CFD) from the perspective of time and computing consumption. The proper orthogonal decomposition (POD) technology has shown its capacity to reconstruct and predict various physical fields. The present study proposes a method based on POD for the reconstruction and prediction of the multiparametri作者: SOBER 時(shí)間: 2025-3-23 09:30
Advances in Cryptology - ASIACRYPT 2009ntrol the quality of aircraft materials and parts processing, and strictly control the design, production and assembly of aircraft, Can control the quality and performance of the whole aircraft assembly, to ensure safety and prolong the life of the aircraft. The use of composite materials not only i作者: cochlea 時(shí)間: 2025-3-23 12:18
Tatsuaki Okamoto,Katsuyuki Takashimame a popular research issue. However, dynamic instability mechanism and control or alleviate methods are still a key issues for the resolve of the un-commanded lateral motions. This exploratory research performed to investigate the cause of non-linearity and the destabilizing mechanism due to the pr作者: ASSAY 時(shí)間: 2025-3-23 14:16 作者: 憤怒事實(shí) 時(shí)間: 2025-3-23 18:33
Advances in Cryptology -- ASIACRYPT 2011ce to that from petroleum-derived jet fuels. SAFs are identified as the best near- to mid-term solution for reducing carbon emissions, with carbon offsetting being the other major carbon mitigation strategy. The primary objective of the research in the paper is to determine if state-of-the-art compu作者: 嚙齒動(dòng)物 時(shí)間: 2025-3-23 23:59
Lecture Notes in Computer Sciencensation heating of the test airflow, and to develop a high-temperature heater; Another is to solve the quality problem of wind tunnel flow field. For the first issue, when the Mach number is less than 10, conventional high Mach aerodynamic test wind tunnels generally use resistance heated heaters as作者: CLAIM 時(shí)間: 2025-3-24 05:47 作者: MERIT 時(shí)間: 2025-3-24 09:15 作者: indices 時(shí)間: 2025-3-24 11:09 作者: Anthology 時(shí)間: 2025-3-24 16:47 作者: 虛弱 時(shí)間: 2025-3-24 21:31
https://doi.org/10.1007/978-3-662-48800-3 and heat transfer in the cavity to ensure the arrangement of heating device in the aircraft cabin. Based on the lattice-Boltzmann method coupled the double distribution function model, the paper adopts D2Q9 velocity discrete model, which has nine different discrete velocity directions. And then cal作者: Restenosis 時(shí)間: 2025-3-25 02:51
Vincent Grosso,Fran?ois-Xavier Standaertaircraft structure and threatens its reliability. The objective of this paper is to propose an efficient engineering approach of residual strength for multi-site damage structures with three types of cracks: non-collinear cracks, inclined cracks and inclined hole-edge cracks. Additionally, the numer作者: 我說不重要 時(shí)間: 2025-3-25 05:34 作者: anchor 時(shí)間: 2025-3-25 10:21
Advances in Cryptology – ASIACRYPT 2015rns on axisymmetric boattail surfaces by a sub-grid measurement technique. The skin-friction results indicate that detailed flow fields on the surface can be obtained when numerical parameters are selected appropriately. The effect of freestream velocity on the skin-friction streamlines and skin-fri作者: URN 時(shí)間: 2025-3-25 15:37
Advances in Cryptology – ASIACRYPT 2015ejection safety. It identifies the practical requirements and primary applications of high-altitude rescue technology within the realm of ejection seat survival. The paper delineates the key factors impacting passenger ejection safety at high altitudes. Furthermore, it summarizes the developmental h作者: asthma 時(shí)間: 2025-3-25 17:30 作者: 放氣 時(shí)間: 2025-3-25 23:04
https://doi.org/10.1007/978-3-662-48800-3ble to hydrogen combustion characteristics. The combustion principles of the proposed micromix element are analyzed, and a parameter-driven micro-mixing chamber design process is established. By combining simulations using Workbench and UG, genetic algorithms and approximate models are employed to o作者: TRAWL 時(shí)間: 2025-3-26 03:59
Front Matteries and their limitations. I then discuss the major theoretical perspectives that guided this research—Social Shaping of Technology (“SST”) (MacKenzie and Wajcman in The Social Shaping of Technology: How the Refrigerator Got Its Hum, Open University Press, Milton Keynes, 1985; Williams and Edge in R作者: 誘使 時(shí)間: 2025-3-26 06:23 作者: Indent 時(shí)間: 2025-3-26 11:53
Research on Lateral Unmatched Nonlinear Control of UAV Based on L1 Adaptive Control Theory,nto question two other regalian missions of the state, at the heart of its digital security: to levy taxes and to mint coins. However, these two areas could also prove to be powerful instruments for regaining our digital security, whether individual or collective. While multinationals use “tradition作者: MAL 時(shí)間: 2025-3-26 13:39 作者: Crumple 時(shí)間: 2025-3-26 20:13 作者: conceal 時(shí)間: 2025-3-26 22:54
Coupling Dynamic Characteristics Analysis of a Dual-Rotor Aeroengine,ures in exploration seismics. In studies of large areas they often make use of the delay time data provided by the International Seismological Centre. Many results have been obtained using P delays. For instance, Spakman (1986) has used 500,000 ISC P delays to derive a tomographic model of the Upper作者: HATCH 時(shí)間: 2025-3-27 04:44 作者: JOG 時(shí)間: 2025-3-27 08:48
Preliminary Exploration of Hypersonic Wind Tunnel Inlet Test Method,rstanding of the topics, it also includes MATLAB-based examples with codes in order to encourage the readers to become more confident of the fundamentals and to gain insights into DSP. Further, it presents real-world signal processing design problems using MATLAB and programmable DSP processors. In 作者: Constant 時(shí)間: 2025-3-27 13:12 作者: 低位的人或事 時(shí)間: 2025-3-27 17:12
Propulsive/Aerodynamic Coupled Characteristics of the Distributed-Propulsion-Wing in Hover and Forwsignals.? The objective of this book is to develop signal processing algorithms using Python. Python is an interpreted, object-oriented high-level programming language widely used in various software development fields such as data science, machine learning, web development and more. .Digital Signal作者: 突變 時(shí)間: 2025-3-27 21:44 作者: 干旱 時(shí)間: 2025-3-27 23:32
Smart Design and Optimization of a Universal and Low-Cost Double-Tailed UAV, Multiple Access, Time Division Multiple Access and Code DivThis book examines signal processing techniques used in wireless communication illustrated by using the Matlab program. The author discusses these techniques as they relate to Doppler spread, Delay spread, Rayleigh and Rician channel modeli作者: 假 時(shí)間: 2025-3-28 02:21 作者: 寬敞 時(shí)間: 2025-3-28 06:20
Kevin S. McCurley,Claus Dieter Zieglerelligent morphing aircraft flying at high speed in large airspace as the research object, aiming at the technical problems that the aircraft is difficult to obtain sufficient deformable flight test data in advance, which leads to the difficulty in predicting the optimal aerodynamic shape under diffe作者: 傳授知識(shí) 時(shí)間: 2025-3-28 13:39 作者: BUCK 時(shí)間: 2025-3-28 16:47
Advances in Cryptology – ASIACRYPT 2007o reconstruct or predict the flow field instead of the POD modes with the maximum eigenvalues. To validate the feasibility of this POD modes selection method, the velocity and pressure distributions around a 2-dimensional aerofoil NACA0012 are adopted as the steady flow field to be reconstructed and作者: 聯(lián)合 時(shí)間: 2025-3-28 19:39 作者: 責(zé)難 時(shí)間: 2025-3-28 23:59 作者: CHIP 時(shí)間: 2025-3-29 04:54 作者: 藥物 時(shí)間: 2025-3-29 08:54
Lecture Notes in Computer Scienceearch in high Mach flight aerodynamic thermal tests. The aerodynamic thermal tests focus on flow field parameters such as enthalpy and pressure, while the requirements for repeatability and uniformity are not as high as those for aerodynamic tests. If a conventional arc heater is directly used as a 作者: verdict 時(shí)間: 2025-3-29 13:52 作者: 騙子 時(shí)間: 2025-3-29 16:03
Advances in Cryptology -- ASIACRYPT 2012mic disturbances, such as the coupling of low-speed wake flow and forced rotational motion, the aerodynamic forces and moments acting on the projectile exhibit strong nonlinear and unsteady characteristics, posing a challenge for accurately predicting the aerodynamic characteristics of the projectil作者: 繁榮地區(qū) 時(shí)間: 2025-3-29 20:43
Soft Analytical Side-Channel Attacks50 to 3150?Hz, moving away from the resonance region. Dynamic response was measured by performing the rotational excitation test and a 60% stress reduction was observed with the PTUPD mounted. Finally, the parametric analysis results reveal that the additional vibration suppression effects is neglig作者: covert 時(shí)間: 2025-3-30 03:16
Ilan Komargodski,Moni Naor,Eylon Yogevrall DPW model is very similar to that between the conventional airfoil and wing. In addition, the outer duct-wing camber influences are mainly manifested in changing the external flow pressure distributions, and the variation trend is consistent with that caused by camber changes of conventional wi作者: 并置 時(shí)間: 2025-3-30 08:04 作者: Nomadic 時(shí)間: 2025-3-30 12:01
Vladimir Kolesnikov,Alex J. Malozemoffin the United States, which has 200 flights and 55 airports. The compact model formulation enables fast computation. This work represents an initial step towards the integration of hydrogen energy fleets into the existing aviation market.作者: judiciousness 時(shí)間: 2025-3-30 14:02 作者: 明確 時(shí)間: 2025-3-30 19:35
Vladimir Kolesnikov,Alex J. Malozemoff the FE model, we also did some optimization works to refine the parameters and make it befit manufacture. Afterwards, the optimized design was manufactured and the total weight was 17.6?kg finally, a very critical but qualified value when compared with the design index. Finally, with ground and fly作者: 神經(jīng) 時(shí)間: 2025-3-30 21:02 作者: MIME 時(shí)間: 2025-3-31 02:44
CFD Modeling of Sustainable Aviation Fuel Sensitivity on Aero-Engine Combustor,作者: 細(xì)微差別 時(shí)間: 2025-3-31 07:26 作者: Bumptious 時(shí)間: 2025-3-31 09:34
Numerical Study of Flow and Heat Transfer in a Cavity by Lattice Boltzmann Method,978-3-642-15591-8作者: 抑制 時(shí)間: 2025-3-31 16:43
Residual Strength Evaluation of Multi-site Damage Structures with Irregular Cracks,978-981-15-3098-2作者: 符合你規(guī)定 時(shí)間: 2025-3-31 20:10 作者: 歌唱隊(duì) 時(shí)間: 2025-4-1 01:45 作者: cruise 時(shí)間: 2025-4-1 05:19
2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) ProceedingsVolume I作者: 懶洋洋 時(shí)間: 2025-4-1 08:49
Front Matterorks in understanding digital disruption in the recording industry. Drawing upon these theoretical approaches, I present a framework of “Socio-technical Constellations of the Digital Recording Industry” to demonstrate a more complete and sophisticated account of the digital recording industry.
