skip to main content

Title: International Symposium on Air Breathing Engines, 7th, Beijing, People's Republic of China, September 2-6, 1985, Proceedings

The symposium presents general topics on nozzle and external flows; gas turbine combustor developments; inlets; mechanical aspects; ramjets; controls, diagnostics, and instrumentation; turbomachinery; combustion stability and modeling; and propulsin systems and test facilities. Other topics include inviscid flow in turbomachinery, operations and monitoring, fuel injection, viscous effects in turbomachinery, unsteady effects in turbomachinery, and combustor performance correlations. Papers are presented on aero gas turbine engines for commercial application, combustion research for gas turbine engines, numerical simulation of self-excited oscillations in a ramjet inlet-diffuser flow, some recent advances in the instrumentation of airbreathing engines, and numerical modeling of afterburner combustion. In addition, consideration is given to procedures for trending aircraft gas turbine engine performance, simultaneous measurement of velocities and particle sizes for injection systems and ramjet combustors, and energy losses of equilibrium three-dimensional boundary layer.
Authors:
;
Publication Date:
OSTI Identifier:
5635263
Report Number(s):
CONF-8509223-
Resource Type:
Conference
Resource Relation:
Conference: 7. international symposium on air breathing engines, Beijing, China, 2 Sep 1985
Publisher:
AIAA,New York, NY
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; GAS TURBINE ENGINES; MEETINGS; RAMJET ENGINES; COMBUSTION CHAMBERS; LEADING ABSTRACT; PLUMES; TECHNOLOGY ASSESSMENT; TEST FACILITIES; TURBOMACHINERY; ABSTRACTS; DOCUMENT TYPES; ENGINES; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY 330100* -- Internal Combustion Engines