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Decade:
1950-1959 (1)
1940-1949 (182)
1920-1929 (1)
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Serial/Series Title:
NACA Wartime Reports (173)
NACA Advanced Confidential Report (3)
NACA Aircraft Circulars (3)
NACA Advanced Restricted Report (2)
NACA Technical Memorandums (1)
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NACA Memorandum Report
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Cooling of Gas Turbines, 2, Effectiveness of Rim Cooling of Blades
An Experimental Investigation of NACA Submerged-Duct Entrances
Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade
Tests of a 1/7-Scale Semispan Model of the XB-35 Airplane in the Langley 19-Foot Pressure Tunnel
Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail with Stub Fuselage and Stub Horizontal Tail
Wind-Tunnel Tests of a 1/5-Scale Semispan Model of the Republic XF-12 Horizontal Tail Surface
Aerodynamic Characteristics of Four Republic Airfoil Sections from Tests in Langley Two-Dimensional Low-Turbulence Tunnels
Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail Incorporating a De-Icing Air Duct
Vibration-response tests of a 1/5-scale model of the Grumman F6F airplane in the Langley 16-foot high-speed tunnel
Some notes on the effects of jet-exit design on static longitudinal stability
The effect of afterbody length of the hydrodynamic stabilit y of a dynamic model of a flying boat : Langley tank model 134
Flight investigation of factors affecting the carburetor ram and nacelle drag of an A-26B airplane
Tests of the jet-motor air-intake duct system on a 1/4-scale stub-wing model of a pursuit-type airplane
Attainment of a straight-line trajectory for a preset guided missile with special reference to effect of wind or target motion
Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam with a mass at its tip
An evaluation of the knock-limited performance of triptane
The effect of ethylene dibromide on the knock-limited performance of leaded and nonleaded S reference fuel
Characteristics of several single- and dual-rotating propellers in negative thrust
Aerodynamic characteristics of several modifications of a 0.45-scale model of the vertical tail of the Curtiss XP-62 airplane
Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel
Wind-tunnel tests of the 0.15-scale powered model of the Fleetwing XBTK-1 airplane : lateral stability and control
Analysis of V-G Records from the SNB-1 Airplane
An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air
Knock-limited performance of six aromatic amines blended with a base fuel in a full-scale aircraft-engine cylinder
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