錢學森文集

《錢學森文集(英文版):海外學術文獻(1938～1956)》內容簡介：ThisvolumecollectsthescientiticworksofTsienHsuc-shenaccomplishedduringhisstayintheUnitedStatesasagraduatestudent，scientistandprolessorandpublishedintheperiodof1938~1956，whentheaeronauticexplorationsteppedfromlow-speedtohigh-speedregimesandastronautictechnologyentereditsinfantstage.Inthesepapers，headdressedandsolvedaseriesofkeyproblemsinaerodynamics，stabilityofshells，rocketballisticsandengineanalyses，etc.，someofwhichwerepath-breaking.Startingfrom1946，withhisstrategicwisdom，TsienHsue-shenmadepioneeringcontributionstosomefields，suchasjetpropulsion，engineeringcybernetics，physicalmechanicsandengineeringsciences，andSOon.Alltheseworksfeaturetheuniquemethodologyofturningbasictheoriesinnaturalscienceintopracticaltoolsintacklingcomplicatedengineeringproblems.Itisworthnotingthathefirstadvocatedthephilosophyofengineeringsciences，whichhasbeenelucidatedandillustratedinthevolumeandprovedtobetheguidelineofinnovativeindustrialdevelopment.Thecollectedworksmightbenefittoitsextensivereadersingettingdeeperinsightintotheacademiccontributions，scientificthoughtsandstudyingstyleofTsienfromvariousviewpoints.

Boundary Layer in Compressible Fluids

Supersonic Flow over an Inclined Body of Revolution

Problems in Motion of Compressible Fluids and Reaction Propulsion

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

Two-DimensionalsubsonicFlow 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 Shdls

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“I．imiting I。ine，’in Mixed Subsonic and Supersonic Flow of Compressible Fluids

Loss in Compressor or Turbine due to Twisted Blades

Lifring-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 ofhypersonicFlows

One-Dimensional Flows of a Gas Characterized by van der Waals Equation of State

Flow Conditions near the Intersection of a Shock Wave with Sorlid Boundary

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

Rockets and Other Thermal J ets 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 J et PropulsionCenter

Influence of Flame Front 0n the Flow Field

Optimum Thrust Programming for a Sounding Rocket

The Emission of Radiation fromdiatomicGases．III．Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300 K and

Atmospheric Pressure

錢學森生平簡介

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