NAS 1.15:103101
|
An expert system to perform on-line controller tuning |
1 |
NAS 1.15:103102
|
Fatigue crack growth in unidirectional metal matrix composite |
1 |
NAS 1.15:103103
|
The vibro-acoustic mapping of low gravity trajectories on a Learjet aircraft |
1 |
NAS 1.15:103104
|
Computational experience with a three-dimensional rotary engine combustion model |
1 |
NAS 1.15:103105
|
Performance of a supercharged direct-injection stratified-charge rotary combustion engine |
1 |
NAS 1.15:103106
|
Efficiency study comparing two helicopter planetary reduction stages |
1 |
NAS 1.15:103107
|
On the use of external burning to reduce aerospace vehicle transonic drag |
1 |
NAS 1.15:103108
|
A test matrix sequencer for research test facility automation |
1 |
NAS 1.15:103109
|
Dynamics of multistage gear transmission with effects of gearbox vibrations |
1 |
NAS 1.15:103110
|
Performance of a 300 Mbps 1:16 serial/parallel optoelectronic receiver module |
1 |
NAS 1.15:103111
|
Computational modeling and validation for hypersonic inlets |
1 |
NAS 1.15:103112
|
Design of a CO₂ laser power control system for a spacelab microgravity experiment |
1 |
NAS 1.15:103113
|
Simplified design procedures for fiber composite structural components/joints |
1 |
NAS 1.15:103114
|
Swept wing ice accretion modeling |
1 |
NAS 1.15:103115
|
Optical measurement of propeller blade deflections in a spin facility |
2 |
NAS 1.15:103116
|
Surface pitting fatigue life of noninvolute, low-contact-ratio gears |
1 |
NAS 1.15:103117
|
A real time neural net estimator of fatigue life |
1 |
NAS 1.15:103118
|
Progression of damage and fracture in composites under dynamic loading |
1 |
NAS 1.15:103119
|
METCAN verification status |
1 |
NAS 1.15:103120
|
Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft |
1 |