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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
42
National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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NACA Research Memorandums
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Atomic Energy Commission Reports
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NACA Technical Reports
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Argonne National Laboratory Reports
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1953
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1953
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Technical Report Archive and Image Library
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The Fabrication of Thorium Tubes
Radiation Damage to Organic Ion-Exchange Materials
The Valve Actuated Pulse Column Design
Effect of Boron Liner on Neutron Background in Cavity
Tests and Application of Differential Pressure Micromanometer to 305 Building Instrumentation
An investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61
The Effects of Extensible Rocket Racks on Lift, Drag, and Stability of a 1/10 Scale Rocket-Boosted Model of the McDonnell XF3H-1 Airplane for a Mach Number Range of 0.60 to 1.34
Effect of Engine and Control Limits on Steady-State and Transient Performance of Turbojet Engine With Variable-Area Exhaust Nozzle
Low-Lift Buffet Characteristics Obtained From Flight Tests of Unswept Thin Intersecting Surfaces and of Thick 35 Degree Sweptback Surfaces
Altitude Investigation of Several Afterburner Configurations for the J40-WE-8 Turbojet Engine
Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9
Free-Jet Investigation of a 20-Inch Ram-Jet Combustor Utilizing High-Heat-Release Pilot Burner
Investigation of a Chromium Plus Aluminum Oxide Metal-Ceramic Body for Possible Gas Turbine Blade Application
Tests in the Ames 40- by 80-Foot Wind Tunnel of Two Airplane Models Having Aspect Ratio 2 Trapezoidal Wings of Taper Ratios 0.33 and 0.20
Lift, drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: comparison of three wings of aspect ratio 2 of rectangular, swept-back and triangular plan form, including effects of thickness distribution
Evaporation and Spreading of Isooctane Sprays in High Velocity Air Streams
Preliminary drag and heat-transfer data obtained from air-launched cone-cylinder test vehicle over Mach number range from 1.5 to 5.18
Jet effects on flow over afterbodies in supersonic stream
Comparative Tensile Strengths at 1200 Degrees F of Various Root Designs for Cermet Turbine Blades
Comparison of ignition delays of several propellant combinations obtained with modified open-cup and small-scale rocket engine apparatus
Lift, drag, and hinge moments at supersonic speeds of an all-movable triangular wing and body combination
Burning rates of single fuel drops and their application to turbojet combustion process
The Effects of Extensible Rocket Racks on Lift, Drag, and Stability of a 1/10-Scale Rocket-Boosted Model of the McDonnell XF3H-1 Airplane for a Mach Number Range of 0.60 to 1.34 : TED No. NACA DE 31
Thermal-Shock Resistance of a Ceramic Comprising 60 Percent Boron Carbide and 40 Percent Titanium Diboride
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