Combustion and Heat Transfer in Gas Turbine Systems. Proceedings of an International Propulsion Symposium Held at the College of Aeronautics, Cranfield, April 1969

Content: 
Already published in this series, Page ii
Front Matter, Page iii
Copyright, Page iv
FOREWORD, Page viii, E.R. NORSTER
THE COMBUSTION SYSTEM FOR THE OLYMPUS 593 CONCORDE ENGINE, Pages 3-17, D.W. HARVEY
THE COMBUSTION SYSTEM FOR THE OLYMPUS 593 CONCORDE ENGINE, Pages 18-19
THE STATISTICAL ANALYSES OF COMBUSTION CHAMBER TEMPERATURE PROFILES, Pages 21-28, R. THOMPSON, A.V. KING
THE STATISTICAL ANALYSES OF COMBUSTION CHAMBER TEMPERATURE PROFILES, Pages 29-30
THE EVOLUTION OF THE RB 162 COMBUSTION SYSTEM FOR V.T.O.L. APPLICATIONS, Pages 33-61, J.R. POYSER, H.B. MOXON
THE EVOLUTION OF THE RB 162 COMBUSTION SYSTEM FOR V.T.O.L. APPLICATIONS, Page 62
SOME COMBUSTION ASPECTS OF PLENUM CHAMBER BURNING, Pages 63-86, A. SOTHERAN
SOME COMBUSTION ASPECTS OF PLENUM CHAMBER BURNING, Pages 87-88
A SURVEY OF ANNULAR VAPORIZING COMBUSTION CHAMBERS, Pages 91-103, E.C. PARNELL, M.R. WILLIAMS
A SURVEY OF ANNULAR VAPORIZING COMBUSTION CHAMBERS, Page 104
IGNITION THEORY AND ITS APPLICATION TO THE ALTITUDE RELIGHTING PERFORMANCE OF GAS TURBINE COMBUSTORS, Pages 105-116, A.H. LEFEBVRE
IGNITION THEORY AND ITS APPLICATION TO THE ALTITUDE RELIGHTING PERFORMANCE OF GAS TURBINE COMBUSTORS, Pages 117-119
PREMIXED PRIMARY ZONE STUDIES USING A MULTIPLE-PORT BAFFLE, Pages 123-143, J.B. JAMIESON
PREMIXED PRIMARY ZONE STUDIES USING A MULTIPLE-PORT BAFFLE, Page 144
THE AIR RECIRCULATION RATIO IN CAN-TYPE GAS TURBINE COMBUSTION CHAMBERS, Pages 145-162, L. VERDUZIO, P. CAMPANARO
THE AIR RECIRCULATION RATIO IN CAN-TYPE GAS TURBINE COMBUSTION CHAMBERS, Page 163
COOLED GAS TURBINE BLADES, Pages 167-181, J.F. BARNES, J.P. EDWARDS
COOLED GAS TURBINE BLADES, Page 182
THEORETICAL ASSESSMENT OF FLAME TUBE TEMPERATURES IN A COMBUSTOR OPERATING AT TYPICAL S.S.T. CONDITIONS, Pages 183-203, M. WHITTAKER
THEORETICAL ASSESSMENT OF FLAME TUBE TEMPERATURES IN A COMBUSTOR OPERATING AT TYPICAL S.S.T. CONDITIONS, Page 204
RADIATION HEAT TRANSFER TO A POROUS SURFACE COOLED BY A TRANSPIRING FLOW, Pages 207-226, I.E. SMITH, M.J. WATTS
RADIATION HEAT TRANSFER TO A POROUS SURFACE COOLED BY A TRANSPIRING FLOW, Pages 227-228
CORRELATION OF DATA AND PREDICTION OF EFFECTIVENESS FROM FILM COOLING INJECTION GEOMETRIES OF A PRACTICAL NATURE, Pages 229-249, G.J. STURGESS
CORRELATION OF DATA AND PREDICTION OF EFFECTIVENESS FROM FILM COOLING INJECTION GEOMETRIES OF A PRACTICAL NATURE, Page 250
CORROSION TESTING OF HIGH-TEMPERATURE GAS TURBINE ALLOYS, Pages 253-289, S.Y. LEE, W.E. YOUNG
CORROSION TESTING OF HIGH-TEMPERATURE GAS TURBINE ALLOYS, Page 290
HOLLOW-CONE LIQUID SPRAY IN UNIFORM AIR STREAM, Pages 291-304, R. MELLOR, N.A. CHIGIER, J.M. BEÉR
HOLLOW-CONE LIQUID SPRAY IN UNIFORM AIR STREAM, Page 305
FUELS FOR AIRCRAFT GAS TURBINE ENGINES, Pages 309-323, A. LEWIS
FUELS FOR AIRCRAFT GAS TURBINE ENGINES, Pages 324-325
LIQUID FUEL ATOMIZERS FOR USE IN GAS TURBINE COMBUSTION MODEL EXPERIMENTS, Pages 327-337, J.J. MACFARLANE
LIQUID FUEL ATOMIZERS FOR USE IN GAS TURBINE COMBUSTION MODEL EXPERIMENTS, Pages 338-339
SOME OBSERVATIONS OF THE ATOMIZING CHARACTERISTICS OF AIR-BLAST ATOMIZERS, Pages 343-355, R. BRYAN, P.S. GODBOLE, E.R. NORSTER
SOME OBSERVATIONS OF THE ATOMIZING CHARACTERISTICS OF AIR-BLAST ATOMIZERS, Pages 356-359
SOME CONSIDERATIONS OF THE MEASUREMENT OF TEMPERATURES WITHIN AIRCRAFT COMBUSTION CHAMBERS, USING A CALORIMETRIC PROBE, Pages 363-379, A.F. SCHLADER, P. ROUILLER, J. ODGERS
SOME CONSIDERATIONS OF THE MEASUREMENT OF TEMPERATURES WITHIN AIRCRAFT COMBUSTION CHAMBERS, USING A CALORIMETRIC PROBE, Pages 380-381
THE MEASUREMENT OF TEMPERATURES AND RADICAL CONCENTRATIONS IN HIGH-TEMPERATURE, FLOWING-GAS STREAMS, Pages 383-405, D.H. COTTON, C.G. HAUPT
THE MEASUREMENT OF TEMPERATURES AND RADICAL CONCENTRATIONS IN HIGH-TEMPERATURE, FLOWING-GAS STREAMS, Page 406
Delegates, Pages 407-408