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National Advisory Committee for Aeronautics Collection
819
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National Advisory Committee for Aeronautics Collection
819
Technical Report Archive and Image Library
819
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NACA Research Memorandums
485
NACA Technical Notes
259
NACA Technical Reports
54
NACA Technical Memorandums
20
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NACA Research Memorandums
485
NACA Technical Notes
259
NACA Technical Reports
54
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1952
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1952
819
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National Advisory Committee for Aeronautics Collection
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Achievement of Continuous Wall Curvature in Design of Two-Dimensional Symmetrical Supersonic Nozzles
Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow
An Approximate Method of Calculating the Deformations of Wings Having Swept, M or W, A, and Swept-Tip Plan Forms
Axisymmetric Supersonic Flow in Rotating Impellers
Behavior of vortex system behind cruciform wings - motions of fully rolled-up vortices
Buckling of rectangular sandwich plates subjected to edgewise compression with loaded edges simply supported and unloaded edges clamped
The Calculated and Measured Performance Characteristics of a Heated-Wire Liquid-Water-Content Meter for Measuring Icing Severity
Calculation of aerodynamic forces on a propeller in pitch or yaw
Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed
Comparison of High-Speed Operating Characteristics of Size 215 Cylindrical-Roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig
Compressive buckling of simply supported curved plates and cylinders of sandwich construction
Concerning the Flow About Ring-Shaped Cowlings of Finite Thickness: Part 1
Design of two-dimensional channels with prescribed velocity distribution along the channel walls 1: relaxation solutions
Detailed Computational Procedure for Design of Cascade Blades With Prescribed Velocity Distributions in Compressible Potential Flows
Direct Measurements of Skin Friction
Ditching Investigation of a 1/12-Scale Model of the Douglas F3D-2 Airplane, TED No. NACA DE 381
Effects of compressibility on the performance of two full-scale helicopter rotors
The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design
Electrical Pressure Integrator
Equal-Strength Design of Tension-Field Webs and Uprights
Estimate of Slip Effect on Compressible Laminar-Boundary-Layer Skin Friction
Experimental Aerodynamic Derivatives of a Sinusoidally Oscillating Airfoil in Two-Dimensional Flow
Experimental Determination of the Effect of Horizontal-Tail Size, Tail Length, and Vertical Location on Low-Speed Static Longitudinal Stability and Damping Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces
Experimental Determination of Time Constants and Nusselt Numbers for Bare-Wire Thermocouples in High-Velocity Air Streams and Analytic Approximation of Conduction and Radiation Errors
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