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NAS 1.10:11-5-58 L
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Analytical and experimental determination of the coupled natural frequencies and mode shapes of a dynamic model of a single-rotor helicopter / |
1 |
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NAS 1.10:11-21-58 W
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Effect of rest periods on fatigue of high-purity aluminum / |
1 |
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NAS 1.10:11-26-58 E
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Comparison of calculated and experimental total-pressure loss and airflow distribution in tubular turbojet combustors with tapered liners / |
1 |
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NAS 1.10:11-27-58 E
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Performance of typical rear-stage axial-flow compressor rotor blade row at three different blade setting angles / |
1 |
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NAS 1.10:11-30-58 A
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Experimental wind-tunnel investigation of the transonic damping-in-pitch characteristics of two wing-body combinations / |
1 |
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NAS 1.10:12-1-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
1 |
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NAS 1.10:12-2-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
1 |
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NAS 1.10:12-3-58 A
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Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and blowing flaps / |
1 |
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NAS 1.10:12-3-58 L
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An analysis of flight-test measurements of the wing structural deformations in rough air of a large flexible swept-wing airplane / |
1 |
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NAS 1.10:12-3-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
1 |
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NAS 1.10:12-4-58 A
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Three-dimensional orbits of Earth satellites, including effects of Earth oblateness and atmospheric rotation / |
1 |
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NAS 1.10:12-4-58 L
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Preliminary measurements of the noise characteristics of some jet-augmented-flap configurations / |
1 |
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NAS 1.10:12-4-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
1 |
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NAS 1.10:12-5-58 W
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Interaction effects produced by jet exhausting laterally near base of ogive-cylinder model in supersonic main stream / |
1 |
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NAS 1.10:12-8-58 E
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NASA reactor facility hazards summary / |
1 |
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NAS 1.10:12-10-58 E
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NASA reactor facility hazards summary / |
1 |
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NAS 1.10:12-13-58 E
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The thermal stability of unsymmetrical dimethylhydrazine / |
1 |
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NAS 1.10:12-14-58 W
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Structure of weak shock waves in a monatomic gas / |
1 |
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NAS 1.10:12-15-58 L
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Free-flight investigation of a rocket-propelled model to determine the aerodynamic heating on a thin, unswept, untapered, multispar, aluminum-alloy wing at Mach numbers up to 2.22 / |
1 |
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NAS 1.10:12-20-58 L
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Investigation of the maximum spin-up coefficients of friction obtained during tests of a landing gear having a static-load rating of 20,000 pounds / |
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