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NAS 1.15:101581
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Characteristic impedance of microstrip lines |
1 |
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NAS 1.15:101582
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Recent activities in aeroservoelasticity at the NASA Langley Research Center |
1 |
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NAS 1.15:101583
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An analytical sensitivity method for use in integrated aeroservoelastic aircraft design |
1 |
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NAS 1.15:101584
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Flutter suppression control law synthesis for the active flexible wing model |
1 |
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NAS 1.15:101585
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A candidate concept for display of forward-looking wind shear information |
1 |
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NAS 1.15:101586-VOL-1
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NASA in-house commercially developed space facility (CDSF) study report concept configuration definition / |
2 |
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NAS 1.15:101587
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Sensitivity analysis of complex coupled systems to second and higher order derivatives |
1 |
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NAS 1.15:101590
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A slow positron beam generator for lifetime studies |
1 |
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NAS 1.15:101591
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O-ring sealing verification for the Space Shuttle red[e]sign Solid Rocket Motor |
1 |
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NAS 1.15:101592
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Structural Mechanics Division research and technology plans for FY 1989 and accomplishments for FY 1988 |
2 |
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NAS 1.15:101594
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S.S. Freedom structural characterization experiment (SCE) node code |
2 |
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NAS 1.15:101595
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Locating damaged members in a truss structure using modal data a demonstration experiment / |
1 |
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NAS 1.15:101596
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Common Graphics Library (CGL). |
1 |
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NAS 1.15:101598
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Inflow measurements made with a laser velocimeter on a helicopter model in forward flight. |
1 |
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NAS 1.15:101599
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Inflow measurements made with a laser velocimeter on a helicopter model in forward flight. |
1 |
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NAS 1.15:101600
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Free-molecule-flow force and moment coefficients of the Aeroassist Flight Experiment vehicle |
1 |
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NAS 1.15:101601
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Results of the round robin on opening-load measurement conducted by ASTM Task Group E24.04.04 on crack closure measurement and analysis / |
1 |
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NAS 1.15:101602
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On the state estimation of structures with second order observers |
1 |
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NAS 1.15:101603
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Alternate space station Freedom configuration considerations to accommodate solar dynamic power |
2 |
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NAS 1.15:101605
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Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data |
1 |
