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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Technical Reports
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NACA Research Memorandums
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NACA Technical Reports
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1950-1959
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1940-1949
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1950-1959
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October
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October
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26th
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National Advisory Committee for Aeronautics Collection
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Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
Full-Scale Wind-Tunnel Tests of a 35 Degree Swept-Wing Fighter Airplane With a Spoiler-Slot-Deflector Lateral Control System
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle
Wing-Flow Study of Pressure-Drag Reduction at Transonic Speed by Projecting a Jet of Air From the Nose of a Prolate Spheroid of Fineness Ratio 6
Analysis of the turbojet engine for propulsion of supersonic fighter airplanes
Stability and Control Measurements Obtained during USAF-NACA Cooperative Flight-Test Program on the X-4 Airplane (USAF No. 46-677)
Some Effects of Blade Trailing-Edge Thickness on Performance of a Single-Stage Axial-Flow Compressor
Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers
Downwash in Vortex Region Behind Rectangular Half-Wing at Mach Number 1.91
Air-flow characteristics of brazed and rolled wire filter cloth for transpiration-cooled afterburners
Investigation at Mach Numbers of 1.62, 1.93, and 2.41 of the Effect of Oscillation Amplitude on the Damping in Pitch of Delta-Wing-Body Combinations
Influence of chemical composition on rupture properties at 1200 degrees F of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition
Full-scale wind-tunnel tests of a 35 degree swept-wing fighter airplane with a spoiler-slot-deflector lateral control system
Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane
A Low-Speed Investigation of a High-Lift Lateral-Control Device Consisting of a Spoiler-Slot-Deflector and a Trailing-Edge Flap on a Tapered 45 Degree Sweptback Wing
Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections
Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane
The Transition Phase in the Take-Off of an Airplane
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