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  • 錢學森文集(1938-1956海外學術文獻英文版)(精)
    該商品所屬分類:外語 -> 英語讀物
    【市場價】
    1609-2332
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    1006-1458
    【介質】 book
    【ISBN】9787313068309
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    內容介紹



    • 出版社:上海交大
    • ISBN:9787313068309
    • 作者:錢學森
    • 頁數:881
    • 出版日期:2011-10-01
    • 印刷日期:2011-10-01
    • 包裝:精裝
    • 開本:16開
    • 版次:1
    • 印次:1
    • 字數:1383千字
    • 李佩主編的《錢學森文集(1938-1956海外學術文獻)》(英文版)編錄科學大師錢學森在美國學習和工作期間(1938-1956)公開發表的論文。那時正值航空從低速走向高速和航天技術從無到有的階段。1946年開始,錢學森以戰略高度發表了不少開創性的論文,包括噴氣推進、工程控制論、物理力學和工程科學等,深刻反映出20世紀正是將自然科學的基本規律轉化為可解決復雜條件下工程問題的科學理論,從而使人類實現航空航天夢,進入數字信息的新時代。
    • 《錢學森文集(1938-1956海外學術文獻)》(英文版)由李佩主編。 《錢學森文集(1938-1956海外學術文獻)》(英文版)內容簡介: This volume collects the scientific works of Tsien Hsue-shen accomplished during his stay in the United States as a graduate student, scientist and professor and published in the period of 1938-1956, when the aeronautic exploration stepped from low-speed to high-speed regimes and astronautic technology entered its infant stage. In these papers, he addressed and solved a series of key problems in aerodynamics, stability of shells, rocket ballistics and engine analyses, etc., some of which were path-breaking. Starting from 1946, with his strategic wisdom, Tsien Hsue-shen made pioneering contributions to some fields, such as jet propulsion, engineering cybernetics, physical mechanics and engineering sciences, and so on. All these works feature the unique methodology of turning basic theories in natural science into practical tools in tackling complicated engineering problems. It is worth noting that he first advocated the philosophy of engineering sciences, which has been elucidated and illustrated in the volume and proved to be the guideline of innovative industrial development. The collected works might benefit to its extensive readers in getting deeper insight into the academic contributions, scientific thoughts and studying style of Tsien from various viewpoints.
    • Boundary Layer in Compressible Fluids
      Supersonic Flow over an Inclined Body of Revolution
      Problems in Motion of Compressible Fluids and Reaction Propulsion
      Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Suc
      Two-Dimensional Subsonic Flow of Compressible Fluids lttsue-shen"
      The Buckling of Spherical Shells by External Pressure
      The Influence of Curvature on the Buckling Characteristics of Structures
      A Method for Predicting the Compressibility Burble
      The Buckling of Thin Cylindrical Shells under Axial Compression
      Buckling of a Column with Non-Linear Lateral Supports
      A Theory for the Buckling of Thin Shells
      Heat Conduction across a Partially Insulated Wall
      On the Design of the Contraction Cone for a Wind Tunnel
      Symmetrical Joukowsky Airfoils in Shear Flow
      The "Limiting Line" in Mixed Subsonic and Supersonic Flow of Compressible Fluids
      Loss in Compressor or Turbine due to Twisted Blades
      Lifting-Line Theory for a Wing in Non-uniform Flow
      Atomic Energy
      Two-Dimensional Irrotational Mixed Subsonic and Supersonic Flow of a Compressible
      Superaerodynamics, Mechanics of Rarefied Gases Hsue-shen Tsien
      Propagation of Plane Sound Waves in Rarefied Gases
      Similarity Laws of Hypersonic Flows
      One-Dimensional Flows of a Gas Characterized by van der Waals Equation of State
      Flow Conditions near the Intersection of a Shock Wave with Solid Boundary
      Lower Buckling Load'in the Non-Linear Buckling Theory for Thin Shells
      Rockets and Other Thermal Jets Using Nuclear Energy
      Engineering and Engineering Sciences
      On Two-Dimensional Non-steady Motion of a Slender Body in a Compressible Fluid
      Wimt-Tunnel Testing Problems in Superaerodynamics Hsue-shen Tsien
      Airfoils in Slightly Supersonic Flow Hsue-shen Tsien and Judson R. Baron
      Interaction between Parallel Streams of Subsonic and Supersonic Velocities
      Research in Rocket and Jet Propulsion
      A Generalization of Alfrey's Theorem for Visco-elastic Media
      Instruction and Research at the Daniel and Florence Guggenheim Jet Propulsion
      Influence of Flame Front on the Flow Field
      Optimum Thrust Programming for a Sounding Rocket
      The Emission of Radiation from Diatomie Gases. III. Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300 K and
      Atmospheric Pressure
      The Transfer Functions of Rocket Nozzles
      A Similarity Law for Stressing Rapidly Heated Thin-Walled Cylinders
      On the Determination of Rotational Line Half-Widths of Diatomic Molecules
      Automatic Navigation of a Long Range Rocket Vehicle
      A Method for Comparing the Performance of Power Plants for Vertical Flight
      Servo-Stabilization of Combustion in Rocket Motors
      Physical Mechanics, A New Field in Engineering Science
      The Properties of Pure Liquids
      Similarity Laws for Stressing Heated Wings
      Take-Off from Satellite Orbit
      Analysis of Peak-Holding Optimalizing Control
      The Poincar~-Lighthill-Kuo Method
      Thermodynamic Properties of Gas at High Temperatures and Pressures
      Thermonuclear Power Plants
      錢學森生平簡介
      後記
      出版說明
     
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