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NAS 1.60:3486
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Reduced dimer production in solar-simulator-pumped continuous wave iodine lasers based on model simulations and scaling and pumping studies |
1 |
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NAS 1.60:3487
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Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer |
1 |
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NAS 1.60:3489
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Evaluation of COSTAR mass handling characteristics in an environment a simulation of the Hubble Space Telescope service mission / |
1 |
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NAS 1.60:3490
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The corrosion protection of several aluminium alloys by chromic acid and sulfuric acid anodizing |
1 |
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NAS 1.60:3491
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Design tool for multiprocessor scheduling and evaluation of iterative dataflow algorithms |
1 |
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NAS 1.60:3494
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A class of stabilizing controllers for flexible multibody systems |
1 |
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NAS 1.60:3496
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Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils |
1 |
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NAS 1.60:3497
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Heavy ion track-structure calculations for radial dose in arbitrary materials |
1 |
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NAS 1.60:3498
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Comparison of exact solution with eikonal approximation for elastic heavy ion scattering |
1 |
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NAS 1.60:3499
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Universal first-order reliability concept applied to semistatic structures |
1 |
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NAS 1.60:3500
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Carbon dioxide and water vapor production at rest and during exercise a report on data collection for the crew and thermal systems division / |
1 |
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NAS 1.60:3501
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Illustrated structural application of universal first-order reliability method |
1 |
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NAS 1.60:3502
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Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 |
1 |
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NAS 1.60:3503
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Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes |
1 |
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NAS 1.60:3506
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Damage tolerance of candidate thermoset composites for use on single stage to orbit vehicles |
1 |
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NAS 1.60:3508
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An inelastic analysis of a welded aluminum joint |
1 |
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NAS 1.60:3512
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Buckling of composite beams CDDF final report : project no. 91-20 / |
1 |
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NAS 1.60:3515
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Study of potential aerodynamic benefits from spanwise blowing at wingtip |
1 |
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NAS 1.60:3516
|
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane |
1 |
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NAS 1.60:3521
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The NASA Langley 16-foot transonic tunnel : historical overview, facility description, calibration, flow characteristics, and test capabilities / |
1 |
