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NAS 1.15:3337
|
Pressure distributions on a rectangular aspect-ratio-6, slotted supercritical airfoil wing with externally blown flaps / |
1 |
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NAS 1.15:3338
|
Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5̊ / |
1 |
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NAS 1.15:3339
|
Effect of tip clearance on performance of small axial hydraulic turbine / |
1 |
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NAS 1.15:3340
|
Thermogravimetric study of reduction of oxides present in oxidized nickel-base alloy powders / |
1 |
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NAS 1.15:3341
|
Performance of low-pressure-ratio low-tip-speed fan stage with blade tip solidity of 0.65 / |
1 |
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NAS 1.15:3342
|
Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7̊ / |
1 |
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NAS 1.15:3344
|
An investigation of correlation between pilot scanning behavior and workload using stepwise regression analysis / |
1 |
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NAS 1.15:3345
|
Performance of inlet stage of transonic compressor / |
1 |
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NAS 1.15:3346
|
Special report writer : a flexible information management systems documentation and users manual / |
1 |
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NAS 1.15:3347
|
Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor / |
1 |
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NAS 1.15:3348
|
Model investigation of inlet plenum flow straightening techniques for altitude test facility / |
1 |
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NAS 1.15:3349
|
Performance of a low-pressure fan stage with reverse flow / |
1 |
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NAS 1.15:3350
|
Effect of slotted casing treatment on performance of a multistage compressor / |
1 |
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NAS 1.15:3351
|
Incidence angle bounds for lip flow separation of the 13.97-centimeter-diameter inlets / |
1 |
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NAS 1.15:3352
|
Potential use of ceramic coating as a thermal insulation on cooled turbine hardware / |
1 |
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NAS 1.15:3353
|
System tests with electric thruster beam and accelerator directly powered from laboratory solar arrays / |
1 |
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NAS 1.15:3356
|
Aerodynamic performance of 0.4066-scale model of JT8D refan stage / |
1 |
|
NAS 1.15:3357
|
Functioning of inorganic/organic battery separators in silver-zinc cells / |
1 |
|
NAS 1.15:3358
|
Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction / |
1 |
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NAS 1.15:3359
|
Model for calculating electrolytic shunt path losses in large electrochemical energy conversion systems / |
1 |
