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NAS 1.10:12-2-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
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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 / |
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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 / |
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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 / |
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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 / |
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NAS 1.10:12-4-58 W
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Heat transfer in the turbulent incompressible boundary layer. |
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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 / |
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NAS 1.10:12-8-58 E
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NASA reactor facility hazards summary / |
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NAS 1.10:12-10-58 E
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NASA reactor facility hazards summary / |
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NAS 1.10:12-13-58 E
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The thermal stability of unsymmetrical dimethylhydrazine / |
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NAS 1.10:12-14-58 W
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Structure of weak shock waves in a monatomic gas / |
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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 / |
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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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NAS 1.10:12-21-58 E
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Experimental investigation of coaxial jet mixing of two subsonic streams at various temperature, Mach number, and diameter ratios for three configurations / |
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NAS 1.10:12-23-58 E
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A study of oxidation of hydrogen based on flashback of hydrogen-oxygen-nitrogen burner flames / |
1 |
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NAS 1.10:12-24-58 E
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Computer program for solving nine-group diffusion equations for cylindrical reactors / |
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NAS 1.10:12-25-58 A
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Boundary-layer-transition measurements on hemispheres of various surface roughnesses in a wind tunnel at Mach numbers from 2.48 to 3.55 / |
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NAS 1.10:12-26-58 A
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Effect of leading-edge sweep and surface inclination on the hypersonic flow field over a blunt flat plate / |
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NAS 1.10:12-28-58 L
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Basic pressure measurements at transonic speeds on a thin 45 sweptback highly tapered wing with systematic spanwise twist variations with wing linear spanwise twist variation / |
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