標(biāo)題: Titlebook: Recent Developments in High-Speed Transport; Selected Contributio Dmitry Yu. Strelets,Oleg N. Korsun Book 2023 The Editor(s) (if applicable [打印本頁] 作者: 投降 時(shí)間: 2025-3-21 18:45
書目名稱Recent Developments in High-Speed Transport影響因子(影響力)
書目名稱Recent Developments in High-Speed Transport影響因子(影響力)學(xué)科排名
書目名稱Recent Developments in High-Speed Transport網(wǎng)絡(luò)公開度
書目名稱Recent Developments in High-Speed Transport網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Recent Developments in High-Speed Transport被引頻次
書目名稱Recent Developments in High-Speed Transport被引頻次學(xué)科排名
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書目名稱Recent Developments in High-Speed Transport年度引用學(xué)科排名
書目名稱Recent Developments in High-Speed Transport讀者反饋
書目名稱Recent Developments in High-Speed Transport讀者反饋學(xué)科排名
作者: 沙文主義 時(shí)間: 2025-3-21 21:21
Recent Developments in High-Speed Transport978-981-19-9010-6Series ISSN 1869-1730 Series E-ISSN 1869-1749 作者: 高原 時(shí)間: 2025-3-22 01:31
Advanced Supersonic Passenger Aircraft Cockpit TechnologiesThe article discusses the design of the cabin of a supersonic passenger aircraft. Modern technologies are considered: multimodal interaction, touch screen displays, synthetic and enhanced vision, technical vision, etc. A cockpit demonstrator designed using the above technologies is presented.作者: Pituitary-Gland 時(shí)間: 2025-3-22 05:52
Methods for Operational Correction of Aircraft Indication Support in Flight TestsIn this paper a method for operational correction of the indication support of subsonic aircraft has been proposed, which includes the technology of simulation of display frames. The simulation station has also been created for operational testing alongside the participation of pilots.作者: Flustered 時(shí)間: 2025-3-22 12:07 作者: anachronistic 時(shí)間: 2025-3-22 15:17
Springer Aerospace Technologyhttp://image.papertrans.cn/r/image/823171.jpg作者: 伸展 時(shí)間: 2025-3-22 17:26 作者: Compassionate 時(shí)間: 2025-3-22 23:15 作者: 吸氣 時(shí)間: 2025-3-23 05:06
Synthesis of a Controller Based on the Principle of Inverse Dynamics and the Online Identification othe independence of roll and yaw motion in a second-generation supersonic transport (SST) with the online identification of a lateral motion mathematical model. The supplementation of the proposed controller with a proportional-integral controller is considered.作者: 捐助 時(shí)間: 2025-3-23 09:04 作者: Pedagogy 時(shí)間: 2025-3-23 10:40
To the Problem of Selecting the Anti-Icing System for the Swept Wing of Supersonic Flight Demonstratts on top and bottom surfaces of wing were defined using iceFoam solver and engineering method. The calculations showed that the total electric power to ensure the operation of the anti-icing system is equal to N?=?13?081 Wt. The efficiency factor characterizing transformation process of electrical energy into heat is equal to about 0.88–0.95.作者: Hypopnea 時(shí)間: 2025-3-23 16:42
realms of low- and high-temperature evaporite evolution. It is aimed at earth science professionals, sedimentologists, oil and gas explorers, mining geologists as well as environmental geologists..978-3-319-13512-0作者: 綠州 時(shí)間: 2025-3-23 19:37
M. Chulkov,A. Volkov realms of low- and high-temperature evaporite evolution. It is aimed at earth science professionals, sedimentologists, oil and gas explorers, mining geologists as well as environmental geologists..978-3-319-13512-0作者: 沙草紙 時(shí)間: 2025-3-23 22:45
1869-1730 this book are researchers working on high-speed transport, postgraduate students, as well as any individuals willing to broaden their knowledge of high-speed aircraft..978-981-19-9012-0978-981-19-9010-6Series ISSN 1869-1730 Series E-ISSN 1869-1749 作者: 愚蠢人 時(shí)間: 2025-3-24 06:01 作者: 燕麥 時(shí)間: 2025-3-24 09:45 作者: Malcontent 時(shí)間: 2025-3-24 14:18
pressure is best estimated from the 24-h mean air temperature and relative humidity. With some error, the average of the maximum and minimum air temperature and relative humidity can be applied to estimate actual vapor pressure. In this study, application of many equations is presented with correla作者: monochromatic 時(shí)間: 2025-3-24 15:51 作者: Jocose 時(shí)間: 2025-3-24 20:18
retically by means of a conceptual transport model or by applying a plausible closure assumption to the transport equations, and only some unknown constants need be determined experimentally. Especially in recent years numerous similarity models for the ABL have been proposed in the literature. This作者: Decimate 時(shí)間: 2025-3-25 00:17 作者: 希望 時(shí)間: 2025-3-25 04:17
O. N. Korsun,A. A. Pirozhkov,E. D. Glukhova,N. V. Skryabikov scale and the evolution at a larger sequential scale depends upon which one of these factors becomes dominant. The general evolution results in a typical sedimentary cycle..The structural behavior of the Hercynian basement controls distribution and sometimes preservation of the depsits. Diagenesis 作者: OPINE 時(shí)間: 2025-3-25 08:15 作者: 潛移默化 時(shí)間: 2025-3-25 15:28
A. Y. Grishina,A. V. Efremov scale and the evolution at a larger sequential scale depends upon which one of these factors becomes dominant. The general evolution results in a typical sedimentary cycle..The structural behavior of the Hercynian basement controls distribution and sometimes preservation of the depsits. Diagenesis 作者: champaign 時(shí)間: 2025-3-25 18:46
V. A. Prodanik,A. V. Efremov scale and the evolution at a larger sequential scale depends upon which one of these factors becomes dominant. The general evolution results in a typical sedimentary cycle..The structural behavior of the Hercynian basement controls distribution and sometimes preservation of the depsits. Diagenesis 作者: 展覽 時(shí)間: 2025-3-25 20:43 作者: 摘要記錄 時(shí)間: 2025-3-26 01:39
O. N. Korsun,S. V. Nikolaev,M. H. Om scale and the evolution at a larger sequential scale depends upon which one of these factors becomes dominant. The general evolution results in a typical sedimentary cycle..The structural behavior of the Hercynian basement controls distribution and sometimes preservation of the depsits. Diagenesis 作者: Pcos971 時(shí)間: 2025-3-26 05:58 作者: Spongy-Bone 時(shí)間: 2025-3-26 11:16 作者: insidious 時(shí)間: 2025-3-26 15:20 作者: yohimbine 時(shí)間: 2025-3-26 17:52
o diapirs and welds (halokinetic breccias) or have acted as décollement surfaces in fold and thrust belts (rauhwacke). All evaporite salt units will ultimately dissolve, many disappear in the diagenetic realm while others may be preserved until they attain metamorphic grades or interact with a magma作者: 長處 時(shí)間: 2025-3-26 21:34
V. S. Gorbovskoy,E. V. Karpov,A. V. Kazhan,A. O. Korunov,A. Y. Nakvasino diapirs and welds (halokinetic breccias) or have acted as décollement surfaces in fold and thrust belts (rauhwacke). All evaporite salt units will ultimately dissolve, many disappear in the diagenetic realm while others may be preserved until they attain metamorphic grades or interact with a magma作者: 催眠 時(shí)間: 2025-3-27 05:01 作者: 污點(diǎn) 時(shí)間: 2025-3-27 07:53 作者: 大酒杯 時(shí)間: 2025-3-27 12:55
System Methodologies for the Design of Human–Machine Interfaces for Advanced Aircraftthe form of a Petri net. This paper gives an example of the development of data input frames using these methods. The work also considers the crew work simulation using Petri nets to obtain crew tasks performance time intervals. This is relevant given that time issues are particularly important for supersonic aircraft.作者: Matrimony 時(shí)間: 2025-3-27 16:43 作者: 小爭吵 時(shí)間: 2025-3-27 21:32 作者: 預(yù)測 時(shí)間: 2025-3-27 23:44 作者: 吸引力 時(shí)間: 2025-3-28 03:16
Long-Term Demand for Supersonic Jets and Role of Supersonic Flight in Air Transportation of the Futudered in the context of other air transportation modes available with account for changes in transportation infrastructure as a whole. Passengers’ perceptions of the advantages of supersonic flight are also an important factor. This paper analyzes the correlation between ticket prices and demand for作者: Tremor 時(shí)間: 2025-3-28 09:48 作者: shrill 時(shí)間: 2025-3-28 12:19
A Method for Constructing a Hybrid Controller for Reconfiguration of On-Board Systems of a Supersonienger aircraft in one hybrid controller. To develop a hybrid controller, a circuit with switching of parametric and non-parametric controllers is used. The choice of method is based on the availability of parametric information about the control object, current disturbances and the required control 作者: Frenetic 時(shí)間: 2025-3-28 14:45 作者: Etymology 時(shí)間: 2025-3-28 20:27 作者: laceration 時(shí)間: 2025-3-29 00:34 作者: 頭盔 時(shí)間: 2025-3-29 03:05 作者: 半圓鑿 時(shí)間: 2025-3-29 10:25 作者: 大都市 時(shí)間: 2025-3-29 12:44 作者: 他一致 時(shí)間: 2025-3-29 16:38 作者: interference 時(shí)間: 2025-3-29 22:25 作者: 商談 時(shí)間: 2025-3-30 01:05
Problems of a Supersonic Business Aircraft Design with Regard to Cabin Noise Requirementsraft cabins is shown and competitively necessary noise levels in the passenger cabin and cockpit are formulated, which need to be guided by when designing an aircraft. The main noise sources are described, and the analysis of available publications on noise in the cabin of a supersonic aircraft of t作者: 脆弱么 時(shí)間: 2025-3-30 04:14 作者: glisten 時(shí)間: 2025-3-30 10:02
1869-1730 eneration supersonic aircraft design to improve the quality This book describes the basic concepts and various aspects of creating a new generation supersonic passenger aircraft. It presents the fundamental and applied problems essential to the design of aircraft of this type. Solutions to the probl作者: Classify 時(shí)間: 2025-3-30 13:09 作者: 歡呼 時(shí)間: 2025-3-30 18:33 作者: 發(fā)炎 時(shí)間: 2025-3-30 23:41
The Comparison of Calculation and Experimental Results of Sonic Boom Characteristics of the Real Airenergy to affect negatively on humans as well as buildings and structures. In this work, the method is presented and applied to estimate sonic boom characteristic on the ground from supersonic aircraft flying with constant supersonic speed at cruise regime and the comparison of calculation and experimental results is performed.