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1950-1959 (4,118)
1940-1949 (1,035)
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NACA Research Memorandums
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An 8-foot axisymmetrical fixed nozzle for subsonic Mach numbers up to 0.99 and for a supersonic Mach number of 1.2
Ability of pilots to control simulated short-period yawing oscillations
Abstracts pertaining to seaplanes
Acceleration characteristics of a turbojet engine with variable-position inlet guide vanes
Acceleration Characteristics of R-3350 Engine Equipped with NACA Injection Impeller
Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212, TED No. NACA 2378
Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed
Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics I : effect of air bleed at compressor outlet
Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics III : effect of turbine stator adjustment
An acceleration schedule control for accelerating a turbojet engine and its use with a speed control
An acceleration schedule control for accelerating a turbojet engine and its use with a speed control
Accelerations in fighter-airplane crashes
An active particle diffusion theory of flame quenching for laminar flames / Dorothy M. Simon and Frank E. Belles
Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Adaptation of Combustion Principles to Aircraft Propulsion, Volume 2, Combustion in Air-Breathing Jet Engines
Adaptation of Combustion Principles to Aircraft Propulsion, Volume I, Basic Considerations in the Combustion of Hydrocarbon Fuels with Air
Additional abstracts pertaining to seaplanes
Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
Additional experimental heat-transfer and durability data on several forced-convection, air-cooled, strut-supported turbine blades of improved design
Additional experiments with flat-top wing- body combinations at high supersonic speeds
Additional fatigue tests on effects of design details in 355-T6 sand-cast aluminum alloy
Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds
Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
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