Collected Works of H. S. Tsien (1938-1956) book cover

Collected Works of H. S. Tsien (1938-1956)

Dr. H. S. Tsien (also known as Dr. Qian Xuesen), is celebrated as the leader of the research that produced China's first ballistic missiles, its first satellite, and the Silkworm anti-ship missile.

This volume collects the scientific works of Dr. H. S. Tsien (also known as Dr. Qian Xuesen) and his co-authors, which published between 1938-1956 when he was studying and working in the United States as a graduate student, scientist and professor, when aeronautic exploration stepped up from low speed to high speed regimes and astronautic technology entered its infant stage.

Audience
Electrical and Electronic Engineers; Mechanical Engineers; Computer Engineers; Intelligent Systems specialists

Hardbound, 900 Pages

Published: March 2012

Imprint: Academic Press

ISBN: 978-0-12-398277-3

Contents

  • 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 Successive Impulses

    Two-Dimensional Subsonic Flow of Compressible Fluids

    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 Fluid and the Upper Critical Mach Number

    Superaerodynamics, Mechanics of Rarefied Gases

    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

    Wind-Tunnel Testing Problems in Superaerodynamics

    Airfoils in Slightly Supersonic Flow

    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 Center

    Influence of Flame Front on the Flow Field

    Optimum Thrust Programming for a Sounding Rocket

    The Emission of Radiation from Diatomic Gases.Ⅲ.Numerical Emissivity

    Calculations for Carbon Monoxide for Low Optical Densities at 300K 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 Poincare-Lighthill-Kuo Method

    Thermodynamic Properties of Gas at High Temperatures and Pressures

    Thermonuclear Power Plants

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