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.
目錄：
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
钱学森生平简介
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