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NAS 1.10:1-6-59 L
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Investigation of spherical-wave-initiated flow fields around bodies / |
1 |
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NAS 1.10:1-7-59 L
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A wind-tunnel investigation of rotor behavior under extreme operating conditions with a description of blade oscillations attributed to pitch-lag coupling / |
1 |
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NAS 1.10:1-9-59 E
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Experimental investigation of expanded duct sections and screens for reducing flow distortions at subsonic flows / |
1 |
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NAS 1.10:1-9-59 L
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Hydrodynamic impact-load alleviation with a penetrating hydro-ski / |
1 |
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NAS 1.10:1-10-59 A
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Two-dimensional, supersonic, linearized flow with heat addition / |
1 |
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NAS 1.10:1-10-59 E
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Pressure drag of axisymmetric cowls having large initial lip angles at mach numbers from 1.90 to 4.90 / |
1 |
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NAS 1.10:1-10-59 L
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A hydrogen peroxide hot-jet simulator for wind-tunnel tests of turbojet-exit models / |
1 |
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NAS 1.10:1-11-59 E
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Experimental investigation of aerodynamic effects of external combustion in airstream below two-dimensional supersonic wing at mach 2.5 and 3.0 / |
1 |
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NAS 1.10:1-15-59 E
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Combustion of various highly reactive fuels in a 3.84-by-10-inch mach 2 wind tunnel / |
1 |
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NAS 1.10:1-15-59 L
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Effects of fuselage nose length and a canopy on the low-speed oscillatory yawing derivatives of a swept-wing airplane model with a fuselage of circular cross section / |
1 |
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NAS 1.10:1-16-59 A
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A numerical method for calculating the wave drag of a configuration form the second derivative of the area distribution of a series of equivalent bodies of revolution / |
1 |
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NAS 1.10:1-16-59 L
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Semiempirical procedure for estimating lift and drag characteristics of propeller-wing-flap configurations for vertical-and short-take-off-and landing airplanes / |
1 |
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NAS 1.10:1-17-59 L
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Analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane operating over a northwestern United States-Alaska route / |
1 |
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NAS 1.10:1-18-59 A
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Subsonic wing loadings on a 45° sweptback-wing and body combination at high angles of attack / |
1 |
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NAS 1.10:1-19-59 A
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Finishing and inspection of model surfaces for boundary-layer-transition tests / |
1 |
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NAS 1.10:1-19-59 E
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Summary of statistical icing cloud data measured over United States and North Atlantic, Pacific, and Arctic oceans during routine aircraft operations / |
1 |
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NAS 1.10:1-20-59 A
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Boundary-layer transition on hollow cylinders in supersonic free flight as affected by Mach number and a screwthread type of surface roughness / |
1 |
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NAS 1.10:1-20-59 L
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Measurements of total hemispherical emissivity of several stably oxidized metals and some refractory oxide coatings / |
1 |
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NAS 1.10:1-21-59 A
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Experimental investigation of the pressure rise required for the incipient separation of turbulent boundary layers in two-dimensional supersonic flow / |
1 |
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NAS 1.10:1-22-59 A
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Pressure distributions at transonic speeds for bumpy and indented midsections of a basic parabolic-arc body / |
1 |
