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National Advisory Committee for Aeronautics Collection
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Longitudinal Frequency-Response Characteristics of the Douglas D-558-I Airplane as Determined From Experimental Transient-Response Histories to Mach Number of 0.90
Comparison of Turbojet-Engine Altitude Performance Characteristics and Ignition Limits With MIL-F-5624A Fuel, Grades JP-3 and JP-4
Method and Graphs for the Evaluation of Air-Induction Systems
Low-speed tests of a free-to-yaw model in two wind tunnels of different turbulence
Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control
Analytical and Experimental Investigation of Fully Developed Turbulent Flow of Air in a Smooth Tube With Heat Transfer With Variable Fluid Properties
Evaluation of three methods for determining dynamic characteristics of a turbojet engine
Dynamic response at altitude of a turbojet engine with variable area exhaust nozzle
A Photographic Study of Freezing of Water Droplets Falling Freely in Air
Flame speeds of methane-air, propane-air, and ethylene-air mixtures at low initial temperatures
Bodies of Revolution for Minimum Drag at High Supersonic Airspeeds
Investigation of the Structural Damping of a Full-Scale Airplane Wing
On Rotational Conical Flow
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
Effect of Aspect Ratio on the Low-Speed Lateral Control Characteristics of Untapered Low-Aspect-Ratio Wings Equipped With Flap and With Retractable Ailerons
Stress Problems in Pressurized Cabins
Coincidence Method Applied to Ion Beam Measurement
Bonding of molybdenum disulfide to various materials to form a solid lubricating film 1: the bonding mechanism
Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail : lateral characteristics
Fatigue strengths of aircraft materials : axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factor of 1.5
Wind-Tunnel Corrections at High Subsonic Speeds Particularly for an Enclosed Circular Tunnel
The similarity law for nonsteady hypersonic flows and requirements for the dynamical similarity of related bodies in free flight
Time Histories of Maneuvers Performed With an F-86A Airplane During Squadron Operations
Reciprocity relations in aerodynamics
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