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Decade:
1940-1949 (47)
1930-1939 (61)
1920-1929 (1)
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Serial/Series Title:
NACA Advanced Confidential Report (15)
NACA Aircraft Circulars (15)
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UNT Libraries Government Documents Department
Serial/Series Title:
NACA Special Report
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Model tests of a wing-duct system for auxiliary air supply
Experimental investigation of a new type of low-drag wing-nacelle combination
Wind-tunnel investigation of several factors affecting the performance of a high-speed pursuit airplane with air-cooled radial engine
Estimated Effect of Ring Cowl on the Climb and Ceiling of an Airplane, Special Report
Definition of Method of Measurement of Supporting and Control Surface Areas, Special Report
The Effect of Surface Irregularities on Wing Drag. I. Rivets and Spot Welds, 1, Rivets and Spot Welds
Method of Determining the Weights of the Most Important Simple Girders
Relative Efficiencies and Design Charts for Various Engine-Propeller Combinations, Special Report
Preliminary Wind-Tunnel and Flight Tests of a Balanced Split Flap, Special Report
The Relative Hydrodynamic Resistance of Various Types of Rivet Heads from Tests of Planning Surfaces, Special Report
Propeller-Design Problems of High-Speed Airplanes, Special Report
Ice Prevention on Aircraft by Means of Impregnated Leather Covers, Special Report
A Study of Transparent Plastics for use on Aircraft. Supplement
Full-Scale Tests of 4- and 6-Blade, Single- and Dual-Rotating Propellers, Special Report
Statistics of the Bureau Veritas
Wind-Tunnel Investigation of Rectangular Air-Duct Entrances in the Leading Edge of an NACA 23018 Wing, Special Report
Full-Scale Tests of Several Propellers Equipped with Spinners, Cuffs, Airfoil and Round Shanks, and NACA 16-Series Sections, Special Report
Accelerations in Landing with a Tricycle-Type Landing Gear
Experimental Determination of Exhaust Gas Thrust, Special Report
Flight Tests on the Lateral Control of an Airplane having a Split Flap which Retracts Ahead of Conventional Ailerons, Special Report
N.A.C.A. Stall-Warning Device
The Effect of Streamlining the Afterbody of an N.A.C.A. Cowling
Profile-Drag Investigation of an Airplane Wing Equipped with Rubber Inflatable De-Icer
The Calculated Effect of Various Hydrodynamic and Aerodynamic Factors on the Take-Off of a Large Flying Boat
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