NAS 1.15:101682
|
A capacitive technique for real-time monitoring polymer coating thickness on carbon filaments during prepregging process |
1 |
NAS 1.15:101683
|
Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990 |
1 |
NAS 1.15:101684
|
Development of a preliminary high-angle-of-attack nose-down pitch control requirement for high-performance aircraft |
1 |
NAS 1.15:101685
|
Task-oriented display design concept and example / |
1 |
NAS 1.15:101686
|
Analysis of the National Transonic Facility mishap |
1 |
NAS 1.15:101687
|
Thermal/structural analysis of the shaft disk region of a fan drive system |
1 |
NAS 1.15:101688
|
Observations of fatigue crack initiation and damage growth in notched titanium matrix composites |
1 |
NAS 1.15:101689
|
The application of active controls technology to a generic hypersonic aircraft configuration |
1 |
NAS 1.15:101692
|
Real-time flight test analysis and display techniques for the X-29A aircraft |
1 |
NAS 1.15:101694
|
Development and use of interactive displays in real-time ground support research facilities |
1 |
NAS 1.15:101695
|
Simulation at Dryden Flight Research Facility from 1957 to 1982 |
1 |
NAS 1.15:101696
|
The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft |
1 |
NAS 1.15:101697
|
Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 |
1 |
NAS 1.15:101698
|
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances |
1 |
NAS 1.15:101700
|
Initial flight test of a ground deployed system for flying qualities assessment |
1 |
NAS 1.15:101701
|
Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 |
1 |
NAS 1.15:101702
|
Preliminary development of an intelligent computer assistant for engine monitoring |
1 |
NAS 1.15:101704
|
A knowledge-based system design/information tool for aircraft flight control systems |
1 |
NAS 1.15:101705
|
Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization |
1 |
NAS 1.15:101706
|
The Aerospace Energy Systems Laboratory hardware and software implementation / |
2 |