NAS 1.15:206906
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Aeroheating predictions for X-34 using an inviscid-boundary layer method |
1 |
NAS 1.15:206913
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Evaluation of heating methods for thermal structural testing of large structures |
1 |
NAS 1.15:206925
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NASA image eXchange (NOX) |
1 |
NAS 1.15:206929
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Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024 |
1 |
NAS 1.15:206930
|
Flight demonstration of integrated airport surface technologies for increased capacity and safety |
1 |
NAS 1.15:206932
|
Technique assessment of the National Full Scale Aerodynamic Complex fan blades repair |
1 |
NAS 1.15:206939
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On the numerical formulation of parametric linear fractional transformation (LFT) uncertainty models for multivariate matrix polynomial problems |
1 |
NAS 1.15:206953
|
Damping mechanisms for microgravity vibration isolation (MSFC Center Director's Discretionary Fund final report, project No. 94-07) / |
1 |
NAS 1.15:206956
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Living together in space the design and operation of the life support systems on the International Space Station / |
1 |
NAS 1.15:206961
|
Advanced seal technology role in meeting next generation turbine engine goals |
1 |
NAS 1.15:206962
|
Friction and wear properties of a-DLC-based functionally gradient nanocomposite coatings |
1 |
NAS 1.15:206963
|
Tunable microwave components for Ku- and K-band satellite communications |
1 |
NAS 1.15:206964
|
Several microstrip-based conductor/thin film ferroelectric phase shifter designs using (YBa₂CU₃O₇₋₈,Au)/SrTiO₃/LaA1O₃ structures |
1 |
NAS 1.15:206965
|
Application of a modified gas chromatograph to analyze space experiment combustion gases on Space Shuttle mission STS-94 |
1 |
NAS 1.15:206969
|
High strain rate deformation modeling of a polymer matrix composite |
1 |
NAS 1.15:206969/
|
High strain rate deformation modeling of a polymer matrix composite |
1 |
NAS 1.15:206971
|
A modified through-flow ware rotor cycle with combustor bypass ducts |
1 |
NAS 1.15:206972
|
Fluids and combustion facility--combustion integrated rack |
1 |
NAS 1.15:206973
|
Fluids and Combustion Facility--fluid integrated rack |
1 |
NAS 1.15:206974
|
Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction |
1 |