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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
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National Advisory Committee for Aeronautics Collection
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NACA Wartime Reports
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NACA Wartime Reports
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Technical Report Archive and Image Library
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Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 14S-T Aluminum Alloy
Hydraulic Characteristics of the NACA Injection Impeller
Investigations on Laminar Boundary-Layer Stability and Transition on Curved Boundaries
The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane
Some Notes on the Effects of Jet-Exit Design on Static Longitudinal Stability
Stability and Control Force Tests of Four- and Six-Unit Wing Designs of Low Aspect Ratio and 20 Degree Triangular Plan Form
Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections
Tests of the Jet-Motor Air-Intake Duct System on a 1/4-Scale Stub-Wing Model of a Pursuit-Type Airplane
Relation Between Fuel Economy and Crank Angle for the Maximum Rate of Pressure Rise
Effect of Engine-Operating Variables and Internal Coolants on Spark-Advance Requirements of a Liquid-Cooled Cylinder
The Effect of Six Aromatic Amines on the Preignition-Limited Performance of 28-R Aviation Fuel in a CFR Engine
Tests of Air Valves for Intermittent-Jet Engines at Speeds of 20 and 25 Cycles Per Second
The Effect of Mach Number on the Aerodynamic Characteristics of a Single-Engine Pursuit Airplane as Determined From Tests of a 1/3-Scale Model
A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation
Comparison of the Knock-Limited Performance of Triptane With 23 Other Purified Hydrocarbons
A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine 1
Effect of Oil Flow to Piston on Piston-Ring Sticking and Oil Consumption in a Single-Cylinder Engine
An Electromagnetic-Analogy Method of Solving Lifting-Surface-Theory Problems
Engine Tests of Pressurized Shunt-Type Cooling Systems for a Liquid-Cooled Engine
An Experimental Investigation of Rectangular Exhaust-Gas Ejectors Applicable for Engine Cooling
Flight Investigation of the Variation of Drag Coefficient With Mach Number for the Bell P-39N-1 Airplane
Flight Tests of an SB2C-3 Airplane With a Production and Tilted Propeller Axis
Flight Tests of Dive-Recovery Flaps on an XP-51 Airplane
Fuel-Evaporation Loss as Determined by the Change in the Specific Gravity of the Fuel in an Aircraft Fuel Tank
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