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National Advisory Committee for Aeronautics Collection
34
Technical Report Archive and Image Library
34
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National Advisory Committee for Aeronautics Collection
34
Technical Report Archive and Image Library
34
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NACA Wartime Reports
25
NACA Memorandum Reports
13
NACA Advanced Restricted Reports
8
NACA Advanced Confidential Reports
4
NACA Technical Reports
4
NACA Restricted Bulletins
2
NACA Technical Memorandums
2
NACA Technical Notes
2
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NACA Wartime Reports
25
NACA Memorandum Reports
13
NACA Advanced Restricted Reports
8
NACA Advanced Confidential Reports
4
NACA Technical Reports
4
NACA Restricted Bulletins
2
NACA Technical Memorandums
2
NACA Technical Notes
2
Year
1945
34
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1945
34
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May
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May
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English
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English
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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1945
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Fuel-Evaporation Loss as Determined by the Change in the Specific Gravity of the Fuel in an Aircraft Fuel Tank
An Experimental Investigation of Rectangular Exhaust-Gas Ejectors Applicable for Engine Cooling
An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 5: Effect of Thermal System on Airplane Cruise Performance
An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 6: Dry-Air Performance of Thermal System at Several Twin- and Single-Engine Operating Conditions at Various Altitudes
Flight Tests of Dive-Recovery Flaps on an XP-51 Airplane
Prediction of Motions of an Airplane Resulting from Abrupt Movement of Lateral or Directional Controls
Effect of Oil Flow to Piston on Piston-Ring Sticking and Oil Consumption in a Single-Cylinder Engine
Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound
A Photoelectric Hygrometer
A general representation for axial-flow fans and turbines
An analysis of life expectancy of airplane wings in normal cruising flight
Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound
Effect of Engine-Operating Variables and Internal Coolants on Spark-Advance Requirements of a Liquid-Cooled Cylinder
Relation Between Fuel Economy and Crank Angle for the Maximum Rate of Pressure Rise
Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward Mach numbers to 0.725 to determine the effects of camber and compressibility on performance
Flight Tests of an SB2C-3 Airplane With a Production and Tilted Propeller Axis
Performance Selection Charts for Gliders and Twin-Engine Tow Planes
Flight Investigation of the Variation of Drag Coefficient With Mach Number for the Bell P-39N-1 Airplane
An Electromagnetic-Analogy Method of Solving Lifting-Surface-Theory Problems
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
Engine Tests of Pressurized Shunt-Type Cooling Systems for a Liquid-Cooled Engine
Tests of Air Valves for Intermittent-Jet Engines at Speeds of 20 and 25 Cycles Per Second
A Method for Correlating the Cooling Data of Liquid-Cooled Engines and Its Application to the Allison V-3420-11 Engine
The Effect of Six Aromatic Amines on the Preignition-Limited Performance of 28-R Aviation Fuel in a CFR Engine
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