內容簡介
《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.
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 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
後記
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