AIAA-2007-1372 PROPULSION SYSTEM CONCEPTS FOR THE PLANETARY SURVEY MISSIONS
AIAA-2007-1341 DESIGN OF A COUNTER-ROTATING TURBINE FOR A HYPERSONIC AIRCRAFT
AIAA-2007-1335 MICRO PRESSURE SENSOR FOR HIGH TEMPERATURE APPLICATIONS
AIAA-2007-1302 AERODYNAMIC IMPROVEMENT OF LOW PRESSURE TURBINE USING 3D VISCOUS FLOW COMPUTATIONS
AIAA-2007-1299 AERO-THERMAL ANALYSIS OF A PARTIALLY SHROUDED AXIAL TURBINE
AIAA-2007-1290 ON-WING DECISION SUPPORT FOR AERO-ENGINE LINE REPLACEABLE UNIT FAULT ISOLATION
AIAA-2007-1240 ADVANCED HEAT EXCHANGERS FOR USE WITH AIRCRAFT ENGINES
AIAA-2007-1230 NUMERICAL SIMULATIONS OF FLUID-STRUCTURE INTERACTIONS USING IMMERSED BOUNDARY METHOD
AIAA-2007-1215 A QUASI-ONE-DIMENSIONAL MODEL FOR AXIAL TURBINES
AIAA-2007-1164 3D FLOW STRUCTURES ADJACENT RECTANGULAR COOLING HOLES
AIAA-2007-1110 EFFECT OF T56 PRESWIRL COOLING MODELLING ON DISC ASSEMBLY TEMPERATURE PREDICTION
AIAA-2007-1338 A RETRO-FIT CONTROL ARCHITECTURE TO MAINTAIN ENGINE PERFORMANCE WITH USAGE
AIAA-2007-1323 A MODEL FOR PREDICTION OF CORNER SEPARATION