Advances in Aeronautical Sciences. Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12–16 September 1960

Content: 
INTERNATIONAL SERIES IN AERONAUTICS AND ASTRONAUTICS, Page ii
Front Matter, Page iii
Copyright, Page iv
CONTENTS — VOLUME 4, Pages ix-xi
INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES, Pages xiii-xiv
PARTICIPATING ORGANIZATIONS, Pages xv-xvi
COMMITTEES AND AUTHORS, Pages xvii-xxi
FOREWORD, Pages xxiii-xxiv, THEODORE VON KÁRMÁN
THE ROLE OF ENTROPY IN THE AERO-SPACE SCIENCES, Pages 1-40, J. ACKERET
POSSIBILITES ET LIMITES ACTUELLES DE LA THEORIE DES ECOULEMENTS HYPERSONIQUES, Pages 41-57, J.-P. GUIRAUD
ON THE USE OF SHOCK TUNNELS FOR RESEARCH ON HYPERSONIC FLOW, Pages 59-86, D.W. HOLDER, D.L. SCHULTZ
ON THE THEORY OF HYPERSONIC FLOW OVER BLUNT-NOSED SLENDER BODIES, Pages 87-102, V.V. SYCHÉV
BEITRÅGE ZUR THEORIE DER DREIDIMENSIONALEN GRENZSCHICHTEN, Pages 103-120, J.A. ZAAT
ON THREE-DIMENSIONAL NON-LINEAR EFFECTS IN THE STABILITY OF PARALLEL FLOWS, Pages 121-142, J.T. STUART
SOME ASPECTS OF BOUNDARY LAYER TRANSITION AT SUBSONIC SPEEDS, Pages 143-160, ITIRO TANI
BOUNDARY LAYER TRANSITION AT THE LEADING EDGE OF THIN WINGS AND ITS EFFECT ON GENERAL NOSE SEPARATION, Pages 161-184, R.A. WALLIS
ÜBER DIE GRENZSCHICHTABLÖSUNG AM ZYLINDER BEI HOHEN GESCHWINDIGKEITEN, Pages 185-206, A. NAUMANN, H. PFEIFFER
GENERAL METHOD OF INTEGRAL RELATIONS AND ITS APPLICATION TO BOUNDARY LAYER THEORY, Pages 207-219, A.A. DORODNITSYN
AIRCRAFT SHAPES AND THEIR AERODYNAMICS FOR FLIGHT AT SUPERSONIC SPEEDS, Pages 221-252, D. KÜCHEMANN
AERODYNAMIC DESIGN OF SWEPT WINGS AND BODIES FOR TRANSONIC SPEEDS, Pages 253-275, R.C. LOCK, E.W.E. ROGERS
THE AERODYNAMIC DESIGN OF SECTION SHAPES FOR SWEPT WINGS, Pages 277-322, H.H. PEARCEY
HYDRODYNAMIK DER ROTIERENDEN FLÜßIGKEITEN, Pages 323-333, A.A. NIKOLSKI
STRESS CORROSION CRACKING IN HIGH STRENGTH STEEL—OR HYDROGEN EMBRITTLEMENT?, Pages 335-356, I. WEIBULL
ETUDE MICROSCOPIQUE DE LA FISSURATION PAR FATIGUE A HAUTE FREQUENCE, Pages 357-372, FRANÇOIS GIRARD
THE NOTCHED FATIGUE PROPERTIES OF HIGH TENSILE STEELS, Pages 373-386, W.A. MORGAN, R.K. BUHR
FATIGUE CRACK PROPAGATION IN LIGHT ALLOY SHEET MATERIAL AND STRUCTURES, Pages 387-408, J. SCHIJVE
JET THRUST, Pages 409-413, L.A. SIMONOV
THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDS, Pages 415-431, CLINTON E. BROWN, F.E. McLEAN, E.B. KLUNKER
SOME EXPERIMENTAL RESULTS OF GENERATING HIGH FREQUENCY OSCILLATING SHOCK-WAVES AND OSCILLATING SHOCK-WAVE BOUNDARY-LAYER INTERACTION AT SUPERSONIC SPEEDS, Pages 433-446, WLADYSLAW FISZDON
SOME CONTRIBUTIONS TO LAMINAR FLAME THEORY, Pages 447-464, GREGORIO MILLAN, IGNACIO DA RIVA
CONTRIBUTION A L'ÉTUDE DE LA COMBUSTION DANS LES FUSÉES A LITHERGOL OU HYBRIDES, Pages 465-496, ANDRE MOUTET, MARCEL BARRERE
THE EFFECT OF A SHOCK WAVE ON A BURNING SOLID PROPELLANT, Pages 497-511, ELLIS M. LANDSBAUM
ELUCIDATION OF COMBUSTION INSTABILITY IN SOLID PROPELLANT ROCKETS, Pages 513-525, SEIICHIRO KUMAGAI
ON THE TRANSONIC FLOW AROUND WING PROFILES AND REVOLUTION BODIES AT ZERO ANGLE OF ATTACK, Pages 527-555, CARLO FERRARI
OPERATIONS RESEARCH IN THE BASIC DESIGN OF YS-11 TRANSPORT AIRPLANE, Pages 557-574, HIDEMASA KIMURA, SHIZUO KIKUHARA, JIRO KONDO
AIRLINE ECONOMICS IN THE TURBINE ERA, Pages 575-592, F.W. KOLK
CONTENTS OF PREVIOUS VOLUMES, Pages 593-596