NAS 1.26:2012-217760
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Process sensitivity, performance, and direct verification testing of adhesive locking features / |
1 |
NAS 1.26:2012-217764
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Model-driven test generation of distributed systems / |
1 |
NAS 1.26:2012-217765
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Modeling and analysis of mixed synchronous/asynchronous systems / |
1 |
NAS 1.26:2012-217766
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Modeling techniques for high dependability protocols and architecture / |
1 |
NAS 1.26:2012-217767
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Pilot test of a novel method for assessing community response to low-amplitude sonic booms / |
1 |
NAS 1.26:2012-217774
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Solution-space screening of a hypersonic endurance demonstrator / |
1 |
NAS 1.26:2012-217777
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Airborne precision spacing for dependent parallel operations interface study / |
1 |
NAS 1.26:2012-217786
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An overview of a trajectory-based solution for en route and terminal area self-spacing : third revision / |
1 |
NAS 1.26:2012-217807
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A computational investigation of gear windage / |
1 |
NAS 1.26:2012-217809
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Noise measurements of the VAIIPR fan / |
1 |
NAS 1.26:2012-217815
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Preliminary aerodynamic investigation of fan rotor blade morphing / |
1 |
NAS 1.26:2013
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Nondestructive testing of Scout rocket motors / |
1 |
NAS 1.26:2013-215450
|
Experimental and analytical characterization of the macromechanical response for triaxial braided composite materials / |
1 |
NAS 1.26:2013-216500
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Microbiological validation of the IVGEN system / |
1 |
NAS 1.26:2013-216502
|
Comprehensive modeling and analysis of rotorcraft variable speed propulsion system with coupled engine/transmission/rotor dynamics / |
1 |
NAS 1.26:2013-216514
|
GRC GSFC TDRSS waveform metrics report / |
1 |
NAS 1.26:2013-217748
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Issues and strategies in solving multidisciplinary optimization problems / |
1 |
NAS 1.26:2013-217812
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Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2012 tests) / |
1 |
NAS 1.26:2013-217820
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Advanced concept studies for supersonic commercial transports entering service in the 2018 to 2020 period : phase I final report / |
1 |
NAS 1.26:2013-217828
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Simulated beam extraction performance characterization of a 50-cm ion thruster discharge / |
1 |