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出版社:上海交大
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ISBN:9787313068309
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作者:錢學森
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頁數:881
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出版日期:2011-10-01
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印刷日期:2011-10-01
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包裝:精裝
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開本:16開
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版次:1
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印次:1
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字數:1383千字
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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。
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《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.
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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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