Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:20230000488 | Proton testing of AMD v1202b system on chip / | 1 |
NAS 1.15:20230001073 | A compendium of technological solution spaces for barrier issues in aerospace / | 1 |
NAS 1.15:20230001707 | Experimental investigation of block-TPS fence/gap roughness effects on transition onset and turbulent heating augmentation at Mach 6 / | 1 |
NAS 1.15:20230001718 | Control architecture for a concept aircraft with a series/parallel partial hybrid powertrain and distributed electric propulsion / | 1 |
NAS 1.15:20230002108 | Competition of failure modes in an additively manufactured disk superalloy / | 1 |
NAS 1.15:20230002218 | Numerical study of solidification crack susceptibility in novel refractory alloy systems / | 1 |
NAS 1.15:20230002220 | Effect of loading rate on the open hole compression strength of quasi-isotropic carbon/epoxy laminates / | 1 |
NAS 1.15:20230003044 | B4C-Al metal matrix composites for extreme space environments / | 1 |
NAS 1.15:20230003630 | H2O electrolysis with impure water source : final report / | 1 |
NAS 1.15/2: | Bibliography of Lewis Research Center technical publications announced in . | 1 |
NAS 1.15/3: | FY ... scientific and technical reports, articles, papers, and presentations. | 1 |
NAS 1.15/4: |
SeaWiFS postlaunch technical report series SeaWIFS postlaunch technical report series. |
2 |
NAS 1.15/5: | Science directorate publications and presentations, January 1-December 31 .. | 1 |
NAS 1.15/6: | NASA's Hall thruster program. | 1 |
NAS 1.15/7: | Research & technology. | 2 |
NAS 1.15/7-2: | Research and technology report. | 1 |
NAS 1.15:7-206271 | Equivalence of fluctuation splitting and finite volume for one-dimensional gas dynamics / | 1 |
NAS 1.15:8 | Aerodynamic characteristics at mach numbers from 1.6 to 2.8 of 74 deg. swept arrow wings with and without camber and twist. | 1 |
NAS 1.15/8: | Research engineering annual report. | 1 |
NAS 1.15:9 | Investigation of the effects of low Reynolds number operation on the performance of a single-stage turbine with a downstream stator. | 1 |