Kooperativer Bibliotheksverbund

UID:

Series Statement: Mathematical surveys and monographs 4

Language: English

Subjects: Mathematics

Keywords: Bewertungstheorie

DOI: 10.1090/surv/004

URL: Volltext  (URL des Erstveröffentlichers)

Author information: Schilling, Otto F. G. 1911-1973

UID:

Format: Online-Ressource (100 p.) , 23 cm

Uniform Title: Mythus von der Geburt des Helden 〈English〉

Content: "The prominent civilized nations, such as the Babylonians, Egyptians, Hebrews, and Hindoos, the inhabitants of Iran and of Persia, the Greeks and the Romans as well as the Teutons and others, all began at an early stage to glorify their heroes, mythical princes and kings, founders of religions, dynasties, empires or cities, in brief their national heroes, in a number of poetic tales and legends. The history of the birth and of the early life of these personalities came to be especially invested with fantastic features, which in different nations even though widely separated by space and entirely independent of each other present a baffling similarity, or in part a literal correspondence. Many investigators have long been impressed with this fact, and one of the chief problems of mythical research still consists in the elucidation of the reason for the extensive analogies in the fundamental outlines of mythical tales, which are rendered still more enigmatical by the unanimity in certain details, and their reappearance in most of the mythical groupings. In this book, we shall first take up the legendary material on which such a psychological interpretation is to be attempted for the first time on a large scale; selecting from the mass of these chiefly biographical hero myths those which are the best known, and some which are especially characteristic. These myths will be given in abbreviated form as far as relevant for this investigation, with statements concerning the provenance. Attention will be called to the most important, constantly recurrent motives by a difference in print"--Introduction. (PsycINFO Database Record (c) 2007 APA, all rights reserved)

Note: Bibliographical footnotes. - Electronic reproduction; Washington, D.C; American Psychological Association; 2005; Available via the World Wide Web; Access limited by licensing agreement; s2005 dcunns

Language: English

URL: Volltext

Author information: Rank, Otto 1881-1939

UID:

Format: Online-Ressource (1238 p) , illustrations, maps, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 11762

Note: A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory, by Clarence W. Matthews [No. 1155], p. 1125 , A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements, by John A. Zaloveik, Lindsay J. Lina, and James P. Trant, Jr. [No. 1145], p. 899 , A special investigation to develop a general method for three-dimensional photoelastic stress analysis, by M.M. Frocht and R. Guernsey, Jr. [No. 1148], p. 963 , A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates, by Herbert F. Hardrath and Lachlan Ohman [No. 1117], p. 213 , A study of inviscid flow about airfoils at high supersonic speeds, by A.J. Eggers, Jr., Clarence A. Syvertson, and Samuel Kraus [No. 1123], p. 339 , A thermodynamic study of the turbine-propeller engine, by Benjamin Pinkel and Irving M. Karp [No. 1114], p. 117 , A vector study of linearized supersonic flow applications to nonplanar problems, by John C. Martin [No. 1143], p. 845 , Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth [No. 1144], p. 879 , Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps, by Jones F. Cahill, William J. Underwood, Robert J. Nuber, and Gail A. Cheesman [No. 1146], p. 913 , An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force, by Simon Ostrach [No. 1111], p. 63 , Analysis of landing-gear behavior, by Benjamin Milwitzky and Francis E. Cook [No. 1154], p. 1077 , Analytical derivation and experimental evaluation of short-bearing approximation for full journal bearings, by George B. DuBois and Fred W. Ocvirk [No. 1157], p. 1199 , Appendices, p. 72 , Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 [degree] of turning, by John D. Stanitz and Leonard J. Sheldrake [No. 1116], p. 193 , Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed, by Herbert C. Nelson and Julian H. Berman [No. 1128], p. 469 , Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings, by Kenneth A. Foss and Franklin W. Diederich [No. 1139], p. 715 , Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings, by Franklin W. Diederich and Kenneth A. Foss [No. 1140], p. 743 , Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow, by Harry L. Runyan and Charles E. Watkins [No. 1150], p. 993 , Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings, by Manuel Stein, J. Edward Anderson, and John M. Hedgepeth [No. 1131], p. 513 , Design of two-dimensional channels with prescribed velocity distributions along the channel walls, by John D. Stanitz [No. 1115], p. 153 , Diffusion of heat from a line source in isotropic turbulence, by Mahinder S. Uberoi and Stanley Corrsin [No. 1142}, p. 815 , Direct measurements of skin friction, by Satish Dhawan [No. 1121], p. 281 , Displacement effect of a three-dimensional boundary layer, by Franklin K. Moore [No. 1124], p. 367 , Dynamics of mechanical feedback-type hydraulic servomotors under inertia loads, by Harold Gold, Edward W. Otto, and Victor L. Ransom [No. 1125], p. 373 , Equations, tables, and charts for compressible flow, by Ames Research staff [No. 1135], p. 611 , Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers, by Ralph W. Stone, Jr. [No. 1136], p. 683 , Experiments to determine neighborhood reactions to light airplanes with and without external noise reduction, by Fred S. Elwell [No. 1156], p. 1155 , Hydrocarbon and nonhydrocarbon derivatives of cyclopropane, by Vernon A. Slabey, Paul H. Wise, and Louis C. Gibbons [No. 1112], p. 81 , Initial results of instrument-flying trials conducted in a single-rotor helicopter, by Almer D. Crim, John P. Reeder, and James B. Whitten [No. 1137], p. 695 , Laminar boundary layer on cone in supersonic flow at large angle of attack, by Franklin K. Moore [No. 1132], p. 533 , List of technical reports, p. III , Mechanism of start and development of aircraft crash fires, by I. Irving Pinkel, G. Merritt Preston and Gerard J. Pesman [No. 1133], p. 546 , Method and graphs for the evaluation of air-induction systems, by George B. Brajinikoff [No. 1141], p. 793 , Method for calculation of laminar heat transfer in air flow around cylinders of arbitrary cross section (including large temperature differences and transpirational cooling), by E.R.G. Eckert and John N.B. Livingood [No. 1118], p. 223 , On the application of transonic similarity rules to wings of finite span, by John R. Spreiter [No. 1153], p. 1055 , On transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1149], p. 981 , One-dimensional analysis of choked-flow turbines, by Robert E. English and Richard H. Cavicchi [No. 1127], p. 451 , Photographic investigation of combustion in a two-dimensional transparent rocket engine, by Donald R. Bellman, Jack C. Humphrey and Theodore Male [No. 1134], p. 599 , Reciprocity relations in aerodynamics, by Max A. Heaslet and John R. Spreiter [No. 1119], p. 253 , Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings, by Dwight G. Moore, Mary A. Mason, and William N. Harrison [No. 1120], p. 269 , Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw, by John D. Bird, Lewis R. Fisher, and Sadie M. Hubbard [No. 1130], p. 495 , Spectrum of turbulence in a contracting stream, by H.S. Ribner and M. Tucker [No. 1113], p. 99 , Study of inadvertent speed increases in transport operation, by Henry A. Pearson [No. 1138], p. 703 , Survey of portions of the chromium-cobalt-nickel- molybdenum quaternary system at 1200 [degrees] C., by Sheldon Paul Rideout and Paul A. Beck [No. 1122], p. 301 , Table of contents, p. II , The effect of blade-section thickness ratios on the aerodynamic characteristics of related full-scale propellers at mach numbers up to 0.65, by Julian D. Maynard and Seymour Steinberg [No. 1126], p. 395 , The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives, by Robert O. Schade and James L. Hassell, Jr. [No. 1151], p. 1001 , The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight, by Frank M. Hamaker, Stanford E. Neice, and Thomas J. Wong [No. 1147], p. 951 , Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies, by Emanuel Schnitzer [No. 1152], p. 1025 , Transverse vibrations of hollow thin-walled cylindrical beams, by Bernard Budiansky and Edwin T. Kruszewski [No. 1129], p. 485 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (1452 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 11595

Note: A comparison of theory and experiment for high-speed free-molecule flow, by Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager [No. 1032], p. 735 , A general integral form of the boundary-layer equation for incompressible flow with an application to the calculation of the separation point of turbulent boundary layers, by Neal Tetervin and Chia Chiao Lin [No. 1046], p. 1067 , A lift-cancellation technique in linearized supersonic-wing theory, by Harold Mirels [No. 1004], p. 65 , A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions, by Richard R. Heldenfels [No. 1043], p. 1019 , A recurrence matrix solution for the dynamic response of aircraft in gusts, by John C. Houbolt [No. 1010], p. 145 , A small-deflection theory for curved sandwich plates, by Manuel Stein and J. Mayers [No. 1008], p. 129 , A study of effects of viscosity on flow over slender inclined bodies of revolution, by H. Julian Allen and Edward W. Perkins [No. 1048.], p. 1103 , A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results, by John D. Bird and Byron M. Jaquet [No. 1031], p. 709 , A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow, by Arthur L. Jones and Alberta Alksne [No. 1052], p. 1211 , A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane, by Leonard Sternfield and Ordway B. Gates, Jr. [No. 1018], p. 291 , An analysis of base pressure at supersonic velocities and comparison with experiment, by Dean R. Chapman [No. 1051], p. 1187 , Analysis of means of improving the uncontrolled lateral motions of personal airplanes, by Marion O. McKinney, Jr. [No. 1035], p. 795 , Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range, by M.H. Lee Wu [No. 1021], p. 359 , Analysis of the effects of boundary-layer control on the take-off and power-off landing performance characteristics of a liaison type of airplane, by Elmer A. Horton, Laurence K. Loftin, Jr., Stanley F. Racisz, and John H. Quinn, Jr. [No. 1057], p. 1353 , Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection, by E. Clinton Wilcox and Arthur M. Trout [No. 1006], p. 97 , Analysis of turbulent free-convection boundary layer on flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 1015], p. 255 , Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions, by Alexander Mendelson and Selwyn Gendler [No. 1005], p. 77 , Buckling of thin-walled cylinder under axial compression and internal pressure, by Hsu Lo, Harold Crate, and Edward B. Schwartz [No. 1027], p. 647 , Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1024], p. 413 , Comparison between theory and experiment for wings at supersonic speeds, by Walter G. Vincenti [No. 1033], p. 757 , Comparison of theoretical and experimental heat-transfer characteristics of bodies of revolution at supersonic speeds, by Richard Scherrer [No. 1055], p. 1301 , Compressive strength of flanges, by Elbridge Z. Stowell [No. 1029], p. 675 , Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume, by P.H. Wise, K.T. Serijan, and I.A. Goodman [No. 1003], p. 55 , Diffusion of chromium in alpha cobalt-chromium solid solutions, by John W. Weeton [No. 1023], p. 397 , Dynamics of a turbojet engine considered as a quasi-static system, by Edward W. Otto and Burt L. Taylor, III [No. 1011], p. 177 , Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow, by Charles E. Watkins [No. 1028], p. 657 , Effect of tunnel configuration and testing technique on cascade performance, by John R. Erwin and James C. Emery [No. 1016], p. 263 , Effects of wing flexibility and variable air lift wing bending moments during landing impacts of a small seaplane, by Kenneth F. Merten and Edgar B. Beck [No. 1013], p. 221 , Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the mach lines, by Kennith L. Goin [No. 1041], p. 937 , Experimental and theoretical studies of area suction for the control of the laminar boundary layer on an NACA 64A010 airfoil, by Albert L. Braslow, Dale L. Burrows, Neal Tetervin, and Fioravante Visconti [No. 1025], p. 433 , Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 [degree] sweptback wing and tail surfaces, by M.J. Queijo and Walter D. Wolhart [No. 1049], p. 1117 , Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a mach number of 1.5, by Dean R. Chapman and Edward W. Perkins [No. 1036], p. 805 , Formulas for the supersonic loading, lift, and drag of flat swept-back wings with leading edges behind the mach lines, by Doris Cohen [No. 1050], p. 1146 , General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions, by Vearl N. Huff, Sanford Gordon, and Virginia E. Morrell [No. 1037], p. 829 , Horizontal tail loads in maneuvering flight, by Henry A. Pearson, William A. McGowan, and James J. Donegan [No. 1007], p. 117 , Influence of chemical composition on rupture properties at 1200 [degrees] F. of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition, by E.E. Reynolds, J.W. Freeman, and A.E. White [No. 1058], p. 1385 , Integrals and integral equations in linearized wing theory, by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller [No. 1054], p. 1267 , Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine, by Burt L. Taylor, III, and Frank L. Oppenheimer [No. 1017], p. 279 , Investigation of fretting by microscopic observation, by Douglas Godfrey [No. 1009], p. 135 , Investigation of separation of the turbulent boundary layer, by G.B. Schubauer and P.S. Klebanoff, National Bureau of Standards [No. 1030], p. 689 , Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65 series wings equipped with full-span slotted flaps, by Jack Fischel and James M. Watson [No. 1034], p. 769 , Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward mach numbers to 0.725 to determine the effects of camber and compressibility on performance, by James B. Delano [No. 1012], p. 189 , Investigation of turbulent flow in a two-dimensional channel, by John Laufer, California Institute of Technology [No. 1053], p. 1247 , Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures, by Leroy V. Humble, Warren H. Lowdermilk, and Leland G. Desmon [No. 1020], p. 343 , NACA investigation of fuel performance in piston-type engines, by Henry C. Barnett [No. 1026], p. 453 , On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid, by Carl Kaplan [No. 1039], p. 909 , Relation between inflammables and ignition sources in aircraft environments, by Wilfred E. Scull [No. 1019], p. 303 , Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane, by Leonard Sternfield [No. 1042], p. 1009 , Spectra and diffusion in a round turbulent jet, by Stanley Corrsin and Mahinder S. Uberoi, Johns Hopkins University [No. 1040], p. 915 , Study of effects of sweep on the flutter of cantilever wings, by J.G. Barmby, H.J. Cunningham, and I.E. Garrick [No. 1014], p. 229 , Supersonic flow around circular cones at angles of attack, by Antonio Ferri [No. 1045], p. 1055 , Table of contents, p. II , Temperature distribution in internally heated walls of heat exchangers composed of non-circular flow passages, by E.R.G. Eckert and George M. Low [No. 1022], p. 381 , The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack, by Antonio Ferri [No. 1044], p. 1039 , The stability of the compression cover of box beams stiffened by posts, by Paul Seide and Paul F. Barrett [No. 1047], p. 1087 , Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds, by John DeYoung [No. 1056], p. 1317 , Wind-tunnel investigation of air inlet and outlet openings on a streamline body, by John V. Becker [No. 1038], p. 887 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (xi, 227 p.) , 23 cm

Series Statement: Bulletin 62

Content: "The decision of the United Nations Educational, Scientific and Cultural Organization (UNESCO) to include the study of tensions affecting international understanding as a major project in its program is a logical consequence of its concern with research and education in the maintenance of peace. Areas of tension between nations that regard themselves as most friendly are commonly evident in the words and actions of both public officials and private citizens. They are the foci of conflict in cold war and open hostility. Understanding of these tensions, fundamental to their relief, is so beclouded by stereotyped thinking, nationalistic feelings, catch phrases, and slogans that the need for objective study of their sources and of procedures for resolving them under the auspices of an international cooperative body such as UNESCO is self-evident. International tensions and the techniques for their relief, however, have received very little direct research attention from social scientists who specialize in problems of social behavior. Traditionally, research in international relations has been mainly the province of historians, students of international law and procedure, and diplomats. More recently, and particularly since the experience of World War II demonstrated the practical utility of scholarly knowledge of foreign areas and peoples, there has been a marked increase in research designed to advance understanding of all parts of the world by area specialists with various disciplinary backgrounds. But as yet sociologists, social psychologists, and social anthropologists--the social scientists most directly concerned with problems of behavior--have done little research on international behavior. The present monograph by Dr. Otto Klineberg is an imaginative and technically skillful ordering and application of scattered and fragmentary products of research on human behavior, so that they may be brought to bear with full force on tensions crucial to peace. Modest in its claims for social science, it points the way to the application of a widening range of knowledge relevant to the reduction of the totality of international tensions. It does not profess definitiveness for existing research techniques, yet it establishes their utility and will stimulate the research needed to give a sounder basis in fact and principle for increasing international understanding and cooperation. Credit is meticulously given to others for their contributions to every section of the work, and it is consequently fitting to say here that Dr. Klineberg has given form and direction to a previously unstructured area of social knowledge"--Foreword. (PsycINFO Database Record (c) 2014 APA, all rights reserved)

Note: Includes bibliographical references and indexes. - Electronic reproduction; Washington, D.C; American Psychological Association; 2014; Available via World Wide Web; Access limited by licensing agreement; s2014 dcunns

Language: English

URL: Volltext