NAS 1.15:2019-219902
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Exploration of failure and potential damage markers in Ti-6A1-4V / |
1 |
NAS 1.15:2019-219933
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A novel reconfigurable GaN based fully solid-state microwave power module for communications/radar applications / |
1 |
NAS 1.15:2019-219935
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Comparison of energy conversion technologies for space nuclear power systems / |
1 |
NAS 1.15:2019-219974
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Characterization of flat-plate heat pipe functionality for fuel cell application / |
1 |
NAS 1.15:2019-219978
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Improvements to an explicit algebraic stress model for turbulent jet mixing predictions / |
1 |
NAS 1.15:2019-219979
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TURBOMAT : a probabilistic turbomachinery aeroelastic analysis tool / |
1 |
NAS 1.15:2019-219982
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Atomic oxygen erosion data from the MISSE 2-8 missions / |
1 |
NAS 1.15:2019-219990
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NASA Glenn Icing Research Tunnel : 2018 change in drop-sizing equations due to change in cloud droplet probe sample area / |
1 |
NAS 1.15:2019-219991
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Optical communication link atmospheric attenuation model / |
1 |
NAS 1.15:2019-219995
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Space communications and navigation validation : extracting data for the Strategic Center for Networking, Integration, and Communications Scheduling Algorithms / |
1 |
NAS 1.15:2019-219999
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Fatigue behavior of coated titanium alloys / |
1 |
NAS 1.15:2019-220004
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NASA innovative advanced concepts (NIAC) phase 1 final report : Venus Landsailer Zephyr / |
1 |
NAS 1.15:2019-220011
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Advanced modular power system electronics enclosure thermal testing / |
1 |
NAS 1.15:2019-220012
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Independent effects of Reynolds number and Mach number on aerodynamics of an iced swept wing / |
1 |
NAS 1.15:2019-220019
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Thermal system sizing comparison of a PEM and solid oxide fuel cell systems on Mars / |
1 |
NAS 1.15:2019-220025
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Weber number tests in the NASA icing research tunnel / |
1 |
NAS 1.15:2019-220029
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Ruggedness evaluation of ASTM international standard test methods for shape memory materials : E3097 standard test method for mechanical uniaxial constant force thermal cycling of shape memory alloys / |
1 |
NAS 1.15:2019-220038
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Tribological performance of PM400 bushings in oscillatory sliding from 25 to 927° C / |
1 |
NAS 1.15:2019-220045
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Transfer-function determination for infinite-tube-probe pressure transducers with application to turbofan core/combustor noise / |
1 |
NAS 1.15:2019-220046
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New test rig to measure alternating current losses of both low and high critical temperature superconductors / |
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