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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
58
Technical Report Archive and Image Library
58
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NACA Research Memorandums
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NACA Technical Notes
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NACA Technical Memorandums
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NACA Technical Reports
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NACA Research Memorandums
31
NACA Technical Notes
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1948
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1948
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National Advisory Committee for Aeronautics Collection
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Ditching Tests of a 1/24-Scale Model of the Lockheed XR60-1 Airplane, TED No. NACA 235
Free-flight investigation of 16-inch diameter supersonic ram-jet unit
High-speed wind-tunnel tests of a 1/78-scale model of the Lockheed YP-80A airplane
Ice protection of turbojet engines by inertia separation of water 1: alternate-duct system
Investigation of the diborane - hydrogen peroxide propellant combination
Aerodynamic Characteristics of Several NACA Airfoil Sections at Seven Reynolds Numbers From 0.7 X 10(Exp 6) to 9.0 X 10(Exp 6)
An exploratory investigation of the relative merits of split and chord-extension flaps on a 45 degrees swept-back wing
Theoretical performance of some rocket propellants containing hydrogen, nitrogen, and oxygen
Preliminary Investigation at a Mach Number of 1.9 and a Reynolds Number of 2,200,000 of Three Ailerons Applicable to the Bell XS-2 Airplane Design
Wind-Tunnel Investigation of the Low-Speed Stability and Control Characteristics of a Model With a Sweptback Vee Tail and a Sweptback Wing
Current Status of Longitudinal Stability
Current Status of Longitudinal Stability
Preliminary investigation of hydrazine as a rocket fuel
Preliminary Results of British Nene II Engine Altitude-Chamber Performance Investigation. I - Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle, 1, Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle
Visual Observations of the Shock Wave in Flight
Preliminary Survey of the Aircraft Fire Problem
Calculated condenser performance for a steam turbine power plant for aircraft
On the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow
Free-Flight Investigation of the Rolling Effectiveness of a Wing-Spoiler Arrangement at High Subsonic, Transonic, and Supersonic Speeds
Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the North American XP-86 Airplane
Performance of 24-Inch Supersonic Axial-Flow Compressor in Air 1: Performance of Compressor Rotor at Design Tip Speed of 1600 Feet Per Second
Qualitative Measurements of Relative Flap Effectiveness at Transonic Speeds on a Series of Five Thin Airfoils With 25-Percent-Chord Flaps and Various Amounts of Sweepback
Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets
Factors Affecting Lateral Stability and Controllability
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