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NAS 1.26:210675
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High pressure regenerative turbine engine 21st century propulsion / |
1 |
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NAS 1.26:210680
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Computational aeroacoustics by the space-time CE/SE method |
1 |
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NAS 1.26:210685
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Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests) |
1 |
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NAS 1.26:210687
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Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel |
1 |
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NAS 1.26:210694
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Detection, tracking and analysis of turbulent spots and other coherent structures in unsteady transition |
1 |
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NAS 1.26:210709
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Mars flyer rocket propulsion risk assessment ARC testing |
1 |
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NAS 1.26:210710
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Mars Flyer rocket propulsion risk assessment Kaiser Marquardt testing / |
1 |
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NAS 1.26:210712
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Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations |
1 |
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NAS 1.26:210713
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Linearized unsteady aerodynamic analysis of the acoustic response to wake/blade-row interaction |
1 |
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NAS 1.26:210715
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Viscoplastic model development to account for strength differential application to aged inconel 718 at elevated temperature / |
1 |
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NAS 1.26:210760
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Development of reliability based life prediction methods for thermal and environmental barrier coatings in ceramic matrix composites |
1 |
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NAS 1.26:210761
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Application of TURBO-AE to flutter prediction aeroelastic code development / |
1 |
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NAS 1.26:210762
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Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep |
1 |
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NAS 1.26:210764
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Heat transfer and flow on the blade tip of a gas turbine equipped with a mean-camberline strip |
1 |
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NAS 1.26:210809
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Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests) |
1 |
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NAS 1.26:210810
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Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade |
1 |
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NAS 1.26:210832
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Fracture tests on thin sheet 2024-T3 aluminum alloy for specimens with and without anti-buckling guides |
1 |
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NAS 1.26:210833
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Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material |
1 |
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NAS 1.26:210834
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Preprocessing for eddy dissipation rate and TKE profile generation |
1 |
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NAS 1.26:210835
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Operational performance of sensor systems used to determine atmospheric boundary layer properties as part of the NASA Aircraft Vortex Spacing System Project |
1 |
