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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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The 7 by 10 Foot Wind Tunnel of the National Advisory Committee for Aeronautics
Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds
Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight
Aircraft Accidents: Methods of Analysis
Altitude-wind-tunnel investigation of compressor performance on J47 turbojet engine
Altitude-Wind-Tunnel Investigation of Westinghouse 19B-2 19B-8, and 19XB-1 Jet-Propulsion Engines, Part 1, Operational Characteristics
An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds
An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver
Analytical and experimental investigation of a temperature-schedule acceleration control for a turbojet engine
The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory
The application of the statistical theory of extreme values to gust-load problems
Axially Symmetric Shapes With Minimum Wave Drag
Calculated Effect of Uranium Distribution on Reflector Control Effectiveness for a Water-Moderated Power Reactor
Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls With Application to Turbine Blade Cooling
The change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds
Combustion of gaseous hydrogen at low pressures in a 35 degree sector of a 28-inch-diameter ramjet combustor
Comparison of National Bureau of Standards ceramic coatings L-7C and A-417 on turbine blades in a turbojet engine
Comparison of Several Methods of Cyclic De-Icing of a Gas-Heated Airfoil
Correlation of the Trim Limits of Stability Obtained for a PB2Y-3 Flying Boat and a 1/8-Size Powered Dynamic Model
Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane
Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having various aspect ratios as determined by flight tests at supersonic speeds
Drag Measurements at Transonic Speeds of NACA 65-009 Airfoils Mounted on a Freely Falling Body to Determine the Effects of Sweepback and Aspect Ratio
Drag of Conical and Circular-Arc Boattail Afterbodies at Mach Numbers From 0.6 to 1.3
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