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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
22
National Advisory Committee for Aeronautics Collection
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1952
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1952
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Technical Report Archive and Image Library
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Hydroxides as Moderator Coolants in Power-Breeder-Reactors
Airborne Radiometric Survey of the East Flank of the Big Horn Mountains, Wyoming and Montana
Cooling Characteristics of an Experimental Tail-Pipe Burner With an Annular Cooling-Air Passage
Empirical Cooling Correlation for an Experimental Afterburner With an Annular Cooling Passage
An investigation of the subsonic speed range of a full-span and a semispan model of a plane wing and of a cambered and twisted wing, all having 45 degrees of sweepback
A Theoretical Investigation of the Effect of a Target Seeker Sensitive to Pitch Attitude on the Dynamic Stability and Response Characteristics of a Supersonic Canard Missile Configuration
Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds
Preliminary investigation of a rectangular supersonic scoop inlet with swept sides designed for low drag at a Mach number of 2.7
Empirical cooling correlation for an experimental afterburner with an annular cooling passage
Hinge-Moment and Other Aerodynamic Characteristics at Transonic Speeds of a Quarter-Span Spoiler on a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3
Pressure Measurements on an Ogive-Cylinder Body at Mach Number 4.04
Altitude Wind Tunnel Investigation of High-Temperature Afterburners
Preliminary investigation of the effects of a paddle balance on the control characteristics at transonic speeds of a tapered 45.58 degrees sweptback wing of aspect ratio 3 having a full-span flap-type control
Low-speed tests of a free-to-yaw model in two wind tunnels of different turbulence
The Effective Downwash Characteristics at Transonic Speeds of a 6-Percent-Thick Wing With 47 Degrees of Sweepback in Combination With a Cylindrical Body as Determined From Force Measurements of a Horizontal Tail
Cooling characteristics of an experimental tail-pipe burner with an annular cooling-air passage
Wind-Tunnel Investigation at High and Low Subsonic Mach Numbers of a Thin Sweptback Wing Having an Airfoil Section Designed for High Maximum Lift
Convection of a pattern of vorticity through a shock wave
Boundary Disturbances in High Explosive Shock Tubes
The Resistivity of Cu₃Au During Neutron Irradiation
Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Plane Triangular Wing of Aspect Ratio 3 With Air-to-Air Missile Models Mounted Externally
Analytical Chemistry Division Quarterly Progress Report for Period Ending September 10, 1951
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