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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Low-Amplitude Damping-in-Pitch Characteristics of Four Tailless Swept Wing-Body Combinations at Mach Numbers From 0.85 to 1.30 as Obtained With Rocket-Powered Models
Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds
Effect of variation in fuel pressure on combustion performance of rectangular ram jet
Effect of three flame-holder configurations on subsonic flight performance of rectangular ram jet over range of altitudes
Investigation of spark gaps subjected to altitude and air velocity conditions
Turbojet combustor efficiency with ceramic-coated liners and with mechanical control of fuel wash on walls
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed 4: effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed
Performance characteristics of canard-type missile with wing-mounted nacelle engines at Mach numbers 1.5 to 2.0
The Longitudinal Stability, Control Effectiveness, and Control Hinge Moment Characteristics Obtained From a Flight Investigation of a Canard Missile Configuration at Transonic and Supersonic Speeds
Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle
Application of Spring Tabs to Elevator Controls
Gust-Tunnel Investigation of the Effect of Leading Edge Separation on the Normal Accelerations Experienced by a 45 Degree Sweptback-Wing Model in Gusts
Investigation at high subsonic speeds of the pressure distributions on a 45 degree sweptback horizontal tail mounted at 50-percent and 100-percent vertical-tail span
Wind-tunnel investigation at low speed of the effects of chordwise wing fences and horizontal-tail position on the static longitudinal stability characteristics of an airplane model with a 35 degree sweptback wing
Comparison of effects of ailerons and combinations of spoiler-slot-deflector arrangements on spin recovery of sweptback-wing model having mass distributed along the fuselage
Analysis of Effects of Inlet Pressure Losses on Performance of Axial-Flow Type Turbojet Engine
The Effect of Some Surface Roughness Elements on the Drag of a Body of Revolution at Supersonic Speeds
Pressure Distribution Over Airfoils With Fowler Flaps
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