Call Number (LC) Title Results
NAS 1.15:112764 Automation of data analysis programs used in the cryogenic characterization of superconducting microwave resonators 1
NAS 1.15:112765 Characterization of hybrid ferroelectric/HTS thin films for tunable microwave components 1
NAS 1.15:112766 Microstructure and phase stability of single crystal NiAl alloyed with Hf and Zr 1
NAS 1.15:112767 Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows 1
NAS 1.15:112768 Soot precursor material visualization via simultaneous LIF-LII and characterization via TEM / 1
NAS 1.15:112769 Progressive fracture of fiber composite build-up structures 1
NAS 1.15:112772 Additional observations of actively forming lava tubes and associated structures, Hawaii 1
NAS 1.15:112791 The influence of the photoionizing radiation spectrum on metal-line ratios in Lyα forest clouds 1
NAS 1.15:112792 Chemical vapor deposited SiC (SCS-0) fiber-reinforced strontium aluminosilicate glass-ceramic composites 1
NAS 1.15:112796 Quality and control of water vapor winds 1
NAS 1.15:112819 Investigation of the effect of two-dimensional cavities on boundary layers in an adverse pressure gradient 1
NAS 1.15:112826 Prediction and verification of ductile crack growth from simulated defects in strength overmatched butt welds a thesis ... / 1
NAS 1.15:112828 New millenium inflatable structures technology 1
NAS 1.15:112830 Tissue culture in microgravity 1
NAS 1.15:112831 A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel 1
NAS 1.15:112832 Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques 1
NAS 1.15:112833 Azimuthal patterns of the radiated sound field from a turbofan model 1
NAS 1.15:112834 Continued development of the discontinuous Galerkin method for computational aeroacoustic applications 1
NAS 1.15:112836 The effects of linear microphone array changes on computed sound exposure level footprints 1
NAS 1.15:112837 Application of interface technology in nonlinear analysis of a stitched/RFI composite wing stub box 1