Collected Works of H. S. Tsien (1938-1956)
By- Tsien H S, Formally chief engineer at Boeing, USA
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.
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 ImpulsesTwo-Dimensional Subsonic Flow of Compressible Fluids
The Buckling of Spherical Shells by External PressureThe Influence of Curvature on the Buckling Characteristics of Structures
A Method for Predicting the Compressibility BurbleThe Buckling of Thin Cylindrical Shells under Axial Compression
Buckling of a Column with Non-Linear Lateral SupportsA Theory for the Buckling of Thin Shells
Heat Conduction across a Partially Insulated WallOn the Design of the Contraction Cone for a Wind Tunnel
Symmetrical Joukowsky Airfoils in Shear FlowThe Limiting Line in Mixed Subsonic and Supersonic Flow of Compressible Fluids
Loss in Compressor or Turbine due to Twisted BladesLifting-Line Theory for a Wing in Non-uniform Flow
Atomic EnergyTwo-Dimensional Irrotational Mixed Subsonic and Supersonic Flow of a Compressible Fluid and the Upper Critical Mach Number
Superaerodynamics, Mechanics of Rarefied GasesPropagation of Plane Sound Waves in Rarefied Gases
Similarity Laws of Hypersonic FlowsOne-Dimensional Flows of a Gas Characterized by van der Waals Equation of State
Flow Conditions near the Intersection of a Shock Wave with Solid BoundaryLower Buckling Load in the Non-Linear Buckling Theory for Thin Shells
Rockets and Other Thermal Jets Using Nuclear EnergyEngineering and Engineering Sciences
On Two-Dimensional Non-steady Motion of a Slender Body in a Compressible FluidWind-Tunnel Testing Problems in Superaerodynamics
Airfoils in Slightly Supersonic FlowInteraction between Parallel Streams of Subsonic and Supersonic Velocities
Research in Rocket and Jet PropulsionA Generalization of Alfreys Theorem for Visco-elastic Media
Instruction and Research at the Daniel and Florence Guggenheim Jet Propulsion CenterInfluence of Flame Front on the Flow Field
Optimum Thrust Programming for a Sounding RocketThe Emission of Radiation from Diatomic Gases.¿.Numerical Emissivity
Calculations for Carbon Monoxide for Low Optical Densities at 300K and Atmospheric PressureThe Transfer Functions of Rocket Nozzles
A Similarity Law for Stressing Rapidly Heated Thin-Walled CylindersOn the Determination of Rotational Line Half-Widths of Diatomic Molecules
Automatic Navigation of a Long Range Rocket VehicleA Method for Comparing the Performance of Power Plants for Vertical Flight
Servo-Stabilization of Combustion in Rocket MotorsPhysical Mechanics, A New Field in Engineering Science
The Properties of Pure LiquidsSimilarity Laws for Stressing Heated Wings
Take-Off from Satellite OrbitAnalysis of Peak-Holding Optimalizing Control
The Poincare-Lighthill-Kuo MethodThermodynamic Properties of Gas at High Temperatures and Pressures
Thermonuclear Power Plants

