《钱学森文集 1938-1956》

Boundary Layer in Compressible Fluids1

Problems in Motion of Compressible Fluids and Reaction Propulsion11

Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses128

Two-Dimensional Subsonic Flow of Compressible Fluids137

The Buckling of Spherical Shells by External Pressure146

The Influence of Curvature on the Buckling Characteristics of Structures154

A Method for Predicting the Compressibility Burble168

The Buckling of Thin Cylindrical Shells Under Axial Compression196

Buckling of a Column wiht Non-Linear Lateral Supports206

A Theory for the Buckling of Thin Shells220

Heat Conduction across a Partially Insulated Wall Hsue-shen Tsien232

On the Design of the Contraction Cone for a Wind Tunnel236

Symmetrical Joukowsky Airfoils in Shear Flow239

The “Limiting Line”in Mixed Subsonic and Supersonic Flow of Compressible Fluids258

Loss in Compressor or Turbine due to Twisted Blades292

Lifting-Line Theory for a Wing in Non-Uniform Flow306

Atomic Energy317

Two-Dimensional lrrotational Mixed Subsonic and Supersonie Flow of a Compressible Fluid and the Upper Critical Mach Number327

Superaerodynamics, Mechanics of Rarefied Gases465

Propagation of Plane Sound Waves in Rarefied Gases477

Similarity Laws of Hypersonic Flows485

One-Dimensional Flows of a Gas Characterized by van der Waal's Equation of State490

Flow Conditions near the Intersection of a Shock Wave with Solid Roundary516

Lower Buckling Load in the Non-Linear Buckling Theory for Thin Shells523

Rockets and Other Thermal Jets Using Nuclear Energy525

Engineering and Engineering Sciences550

On Two-Dimensional Non-Steady Motion of a Slender Body in a Compressible Fluid564

Wind-Tunnel Testing Problems in Superaerodynamics576

Airfoils in Slightly Supersonic Flow584

Interaction between Parallel Streams of Subsonic and Supersonic Velocities592

Research in Rocket and Jet Propulsion606

A Generalization of Alfrey's Theorem for Visco-Elastic Media611

Instruction and Research at the Daniel and Florence Guggenheim Jet Propulsion Center614

Influence of Flame Front on the Flow Field628

Optimum Thrust Programming for a Sounding Rocket635

The Emission of Radiation from Diatomic Gases, Ⅲ.Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300°K and Atmospheric Pressure644

The Transfer Functions of Rocket Nozzles652

A Similarity Law for Stressing Rapidly Heated Thin-Walled Cylinders657

On the Determination of Rotational Line Half-Widths of Diatomic Molecules664

Automatic Navigation of a Long Range Rocket Vehicle666

A Method for Comparing the Performance of Power Plants for Vertical Flight674

Servo-Stabilization of Combustion in Rocket Motors678

Physical Mechanics,A New Field in Engineering Science686

The Properties of Pure Liquids690

Similarity Laws for Stressing Heated Wings699

Supersonic Flow over an Inclined Body of Revolution7

Take-Off from Satellite Orbit710

Analysis of Peak-Holding Optimalizing Control714

The Poincare-Lighthill-Kuo Method724

Thermodynamic Properties of Gas at High Temperatures and Pressures793

Thermonuclear Power Plants796

钱学森生平简介802

后记810