NAS 1.26:212099
PREDICTING MODES OF THE UNSTEADY VORTICITY FIELD NEAR THE TRAILING EDGE OF A BLADE... NASA/CR--2003-212099... NATIONAL AERONAUTICS AND SPACE
0830-H-14
20030490M
20031020
NAS 1.26:212106
TURBO/SCISEAL SEALS ANALYSIS METHODOLOGY FOR TIME-ACCURATE ANALYSIS OF COUPLED SEALS, SECONDARY AND POWERSTREAM FLOW..., NASA/CR--2003-21210
NAS 1.26:212121
THE FILTERED ABEL TRANSFORM AND ITS APPLICATION IN COMBUSTION DIAGNOSTICS... NASA/CR--2003-212121... NATIONAL AERONAUTICS AND SPACE ADMINIST
NAS 1.26:212122
ATOMIC-SCALE MODELING OF THE STRUCTURE AND DYNAMICS OF DISLOCATIONS IN COMPLEX ALLOYS AT HIGH TEMPERATURES... NASA/CR--2003-212122... NATION
NAS 1.26:212123
JET NOISE PHYSICS AND MODELING USING FIRST-PRINCIPLES SIMULATIONS... NASA/CR--2003-212123... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212179
DOPPLER GLOBAL VELOCIMETRY AT NASA GLENN RESEARCH CENTER: SYSTEM DISCUSSION AND RESULTS... NASA/CR--2003-212179... NATIONAL AERONAUTICS AND
NAS 1.26:212190
ANALYSIS OF THE EFFECT OF SURFACE MODIFICATION ON POLYIMIDE COMPOSITES COATED WITH EROSION RESISTANT MATERIALS... NASA/CR--2003-212190... NA
NAS 1.26:212191
THRUST AUGMENTATION MEASUREMENTS USING A PULSE DETONATION ENGINE EJECTOR... NASA/CR--2003-212191... NATIONAL AERONAUTICS AND SPACE ADMINISTR
NAS 1.26:212193
THREE DIMENSIONAL NUMERICAL SIMULATION OF ROCKET-BASED COMBINED-CYCLE ENGINE RESPONSE DURING MODE TRANSITION..., NASA/CR--2003-212193... NAT
NAS 1.26:212194
MODELING OF HIGH-STRAIN-RATE DEFORMATION, FRACTURE, AND IMPACT BEHAVIOR OF ADVANCED GAS TURBINE ENGINE MATERIALS..., NASA/CR--2003-212194 ..
NAS 1.26:212197
A DESIGN METHODOLOGY FOR RAPID IMPLEMENTATION OF ACTIVE CONTROL SYSTEMS ACROSS LEAN DIRECT INJECTION COMBUSTER..., NASA/CR--2003-212197... N
NAS 1.26:212198
NANOPOROUS SILICON CARBIDE FOR NANOELECTROMECHANICAL SYSTEMS APPLICATIONS... NASA/CR--2003-212198... NATIONAL AERONAUTICS AND SPACE ADMINIST
NAS 1.26:212199
AN EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION OF OSCILLATING AIRFOIL UNSTEADY AERODYNAMICS AT LARGE MEAN INCIDENCE... NASA/CR--2003-212199
NAS 1.26:212202
SUBGRID COMBUSTION MODELING FOR THE NEXT GENERATION NATIONAL COMBUSTION CODE... NASA/CR--2003-212202... NATIONAL AERONAUTICS AND SPACE ADMIN
NAS 1.26:212210
FLAME SPRAY STRAIN GAGES WITH IMPROVED DURABILITY AND LIFETIMES... NASA/CR--2003-212210... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212293
SULFUR OXIDATION AND CONTRAIL PRECURSOR CHEMISTRY... NASA/CR--2003-212293... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212294
ENHANCED DESIGN OF TURBO-JET LPT BY SEPARATION CONTROL USING PHASE PLASMA ACTUATORS... NASA/CR--2003-212294... NATIONAL AERONAUTICS AND SPAC
NAS 1.26:212306
XENON SPUTTER YIELD MEASUREMENTS FOR ION THRUSTER MATERIALS... NASA/CR--2003-212306... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212309
ULTRA-EFFICIENT ENGINE DIAMETER STUDY... NASA/CR--2003-212309... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212323
TURBOFAN NOISE PROPAGATION AND RADIATION AT HIGH FREQUENCIES... NASA/CR--2003-212323... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
NAS 1.26:212350
COMPARISON OF MARS AIRCRAFT PROPULSION SYSTEMS... NASA/CR--2003-212350... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION