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钱学森文集  1938-1956
钱学森文集  1938-1956

钱学森文集 1938-1956PDF电子书下载

数理化

  • 电子书积分:22 积分如何计算积分?
  • 作 者:钱学森著;王寿云编
  • 出 版 社:北京:科学出版社
  • 出版年份:1991
  • ISBN:7030027118
  • 页数:810 页
图书介绍:本书收集了钱学森同志在美国从事科学研究工作期间用英文完成的51篇科学论文。
《钱学森文集 1938-1956》目录
标签:文集

Boundary Layer in Compressible Fluids 1

Problems in Motion of Compressible Fluids and Reaction Propulsion 11

Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses 128

Two-Dimensional Subsonic Flow of Compressible Fluids 137

The Buckling of Spherical Shells by External Pressure 146

The Influence of Curvature on the Buckling Characteristics of Structures 154

A Method for Predicting the Compressibility Burble 168

The Buckling of Thin Cylindrical Shells Under Axial Compression 196

Buckling of a Column wiht Non-Linear Lateral Supports 206

A Theory for the Buckling of Thin Shells 220

Heat Conduction across a Partially Insulated Wall Hsue-shen Tsien 232

On the Design of the Contraction Cone for a Wind Tunnel 236

Symmetrical Joukowsky Airfoils in Shear Flow 239

The “Limiting Line”in Mixed Subsonic and Supersonic Flow of Compressible Fluids 258

Loss in Compressor or Turbine due to Twisted Blades 292

Lifting-Line Theory for a Wing in Non-Uniform Flow 306

Atomic Energy 317

Two-Dimensional lrrotational Mixed Subsonic and Supersonie Flow of a Compressible Fluid and the Upper Critical Mach Number 327

Superaerodynamics, Mechanics of Rarefied Gases 465

Propagation of Plane Sound Waves in Rarefied Gases 477

Similarity Laws of Hypersonic Flows 485

One-Dimensional Flows of a Gas Characterized by van der Waal's Equation of State 490

Flow Conditions near the Intersection of a Shock Wave with Solid Roundary 516

Lower Buckling Load in the Non-Linear Buckling Theory for Thin Shells 523

Rockets and Other Thermal Jets Using Nuclear Energy 525

Engineering and Engineering Sciences 550

On Two-Dimensional Non-Steady Motion of a Slender Body in a Compressible Fluid 564

Wind-Tunnel Testing Problems in Superaerodynamics 576

Airfoils in Slightly Supersonic Flow 584

Interaction between Parallel Streams of Subsonic and Supersonic Velocities 592

Research in Rocket and Jet Propulsion 606

A Generalization of Alfrey's Theorem for Visco-Elastic Media 611

Instruction and Research at the Daniel and Florence Guggenheim Jet Propulsion Center 614

Influence of Flame Front on the Flow Field 628

Optimum Thrust Programming for a Sounding Rocket 635

The Emission of Radiation from Diatomic Gases, Ⅲ.Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300°K and Atmospheric Pressure 644

The Transfer Functions of Rocket Nozzles 652

A Similarity Law for Stressing Rapidly Heated Thin-Walled Cylinders 657

On the Determination of Rotational Line Half-Widths of Diatomic Molecules 664

Automatic Navigation of a Long Range Rocket Vehicle 666

A Method for Comparing the Performance of Power Plants for Vertical Flight 674

Servo-Stabilization of Combustion in Rocket Motors 678

Physical Mechanics,A New Field in Engineering Science 686

The Properties of Pure Liquids 690

Similarity Laws for Stressing Heated Wings 699

Supersonic Flow over an Inclined Body of Revolution 7

Take-Off from Satellite Orbit 710

Analysis of Peak-Holding Optimalizing Control 714

The Poincare-Lighthill-Kuo Method 724

Thermodynamic Properties of Gas at High Temperatures and Pressures 793

Thermonuclear Power Plants 796

钱学森生平简介 802

后记 810

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