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National Advisory Committee for Aeronautics
Books by Publisher: National Advisory Committee for Aeronautics
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Effect of Chord Size on Weight and Cooling Characteristics of Air-Cooled Turbine Blades (NACA TN 3923)
Jack; Schum, Eugene; Curren, Arthur Esgar
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Effect of Diameter of closed-End Coolant Passages on natural-Convection Water Cooling of gas-Turbine blades: NACA Research Memorandum NO. E55J18a
Arthur N. & Zalabak, Charles F. Curren
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Axial-flow fan and compressor blade design data at 52.5 ÌŠstagger and further verification of cascade data by rotor tests (National Advisory Committee for Aeronautics technical note)
Seymour M Bogdonoff
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The NACA Mixture Analyzer and Its Application to Mixture-Distribution Measurement in Flight Technical Note No. 1238
Harold C.; Meem, J. Lawrence Jr.; Scadron, Marvin D.; Colnar, Anthony Gerrish
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Wartime Reports; E 61-80: 15 reports
Numerous Authors
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A General Representation for Axial-Flow Fans and Turbines (Report No. 814)
National Advisory Committee for Aeronautics
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Methods for Rapid Graphical Evaluation of Cooled or uncooled Turbojet and Turboprop Engine or Component Performance (Effects of Variable Heat Included) (NACA TN 3335)
Jack; Ziemer, Robert Esgar
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An Electromagnetic Flowmeter for Rocket Research Research Memorandum RM No. E50L12
Leonard; Coss, Bert A.; Daykin, Donald R. Jaffe
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The soap-bubble method of studying the combustion of mixtures of CO and O² (Report / National Advisory Committee for Aeronautics)
Ernest F Fiock
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TECHNICAL NOTES: (NACA) NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. No. 320 (Jacobs) The Draga and Interference oa a Nacelle in the Presence of a wing; No. 321(Karman) The impact on seaplane floats during landing; No. 322; 323; 324; 325; 326; 327; 328.
Various
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Characteristics of a Wedge with Various Holder Configurations for Static-Pressure Measurements in Subsonic Gas Streams Research Memorandum RM No. E51G09
Clarence C.; Krause, Lloyd N. Gettelman
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National Advisory Committee for Aeronautics Report 1336 an Investigation of Single-and Dual-rotation Propellers at Positive and Negative Thrust and in Combination with an NACA 1-Series D-type Cowling at Mach Numbers Up to 0.84
Reynolds Robert M et al
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Comparison of Performance of Two Aerodynamically Similar 14-Inch-diameter Single-Stage Compressor Rotors of Different Chord length: NACA Research Memorandum NO. E57I03
Marvin I. Kussoy
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Discharge characteristics of a high speed fuel injection engine (Technical notes / National Advisory Committee for Aeronautics)
Robertson Matthews
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Static thrust analysis of the lifting airscrew
Montgomery Knight
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