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NACA Technical Reports
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1932
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General Potential Theory of Arbitrary Wing Sections
Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 3: Ordinary Ailerons Rigged Up 10 Degrees When Neutral
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 4: floating tip ailerons on rectangular wings
The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays
The Effect of Humidity on Engine Power at Altitude
The Effect of Multiple Fixed Slots and a Trailing-Edge Flap on the Lift and Drag of a Clark Y Airfoil
Wind-Tunnel Tests of a Clark Y Wing With a Narrow Auxiliary Airfoil in Different Positions
Characteristics of Clark Y airfoils of small aspect ratios
Force measurements on a 1/40-scale model of the U. S. Airship "Akron"
Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines
Measurements of flow in the boundary layer of a 1/40-scale model of the U. S. Airship "Akron"
Lift and drag characteristics and gliding performance of an autogiro as determined in flight
Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine
The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages
Experiments on the distribution of fuel in fuel sprays
Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 5: Spoilers and Ailerons on Rectangular Wings
The Mechanism of Atomization Accompanying Solid Injection
A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests
A comparison between the theoretical and measured longitudinal stability characteristics of an airplane
Pressure-distribution measurements on the hull and fins of scale model of the U. S. Airship "Akron"
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 6: skewed ailerons on rectangular wings
Working Charts for the Determination of the Lift Distribution Between Biplane Wings
Airfoil section characteristics as affected by protuberances
Static thrust of airplane propellers
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