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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
12
Technical Report Archive and Image Library
12
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1948
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1948
12
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National Advisory Committee for Aeronautics Collection
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1948
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Investigation of Effects of Several Fuel-Injection Locations on Operational Performance of a 20-Inch Ram Jet
Notes on Geared Tabs at Supersonic Speeds
Experimental investigation of thrust augmentation of axial-flow-type 4000-pound-thrust turbojet engine by water and alcohol injection at compressor inlet
High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane: Longitudinal Stability and Control of the D-558-1
Ice protection of turbojet engines by inertia separation of water 2: single-offset-duct system
Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds From Tests by the NACA Wing-Flow Method
Some preliminary results in the determination of aerodynamic derivatives of control surfaces in the transonic speed range by means of a flush-type electrical pressure cell
Yaw Characteristics of a 52 Degree Sweptback Wing of NACA 64(Sub 1)-112 Section With a Fuselage and With Leading-Edge and Split Flaps at Reynolds Numbers From 1.93 X 10(Exp 6) to 6.00 X 10(Exp 6)
Ice protection of turbojet engines by inertia separation of water 3: annular submerged inlets
Internal-Film Cooling of Rocket Nozzles
An experimental investigation of the design variables for NACA submerged duct entrances
Tank Tests of a Powered Model of a Compression Plane, NACA Model 171A-2
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