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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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National Advisory Committee for Aeronautics Collection
16
Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Technical Notes
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NACA Research Memorandums
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NACA Technical Notes
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1950-1959
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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Cooling Characteristics of an Experimental Tail-Pipe Burner With an Annular Cooling-Air Passage
The Aerodynamic Characteristics of Airfoils at Negative Angles of Attack
Free-flight performance of 16-inch diameter supersonic ram-jet units 4: performance of ram-jet units designed for combustion chamber inlet Mach number of 0.21 at free-stream Mach number of 1.6 over a range flight conditions
Wind-Tunnel Investigation at Mach Numbers From 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 With Leading- and Trailing-Edge Flaps - Flaps Deflected in Combination
Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps deflected
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
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
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
Effectiveness at transonic speeds of flap-type ailerons for several spanwise locations on a 4-percent-thick sweptback-wing-fuselage model with and without tails
Zero-Lift Drag of a Large Fuselage Cavity and a Partially Submerged Store on a 52.5 Degree Sweptback-Wing-Body Configuration as Determined From Free-Flight Tests at Mach Numbers of 0.7 to 1.53
Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model having double slotted flaps and spoilers
Rocket Thrust Variation With Foamed Liquid Propellants
Minimum Specific Fuel Consumption of a Liquid-Cooled Multicylinder Aircraft Engine as Affected by Compression Ratio and Engine Operating Conditions
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