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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Research Memorandums
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May
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National Advisory Committee for Aeronautics Collection
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Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure
Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow
Comparison of the aerodynamic characteristics at transonic speeds of a plane wing and a cambered and twisted wing, both having 45 degrees of sweepback and an aspect ratio of 6
Study of the Pressure Rise Across Shock Waves Required to Separate Laminar and Turbulent Boundary Layers
Aerodynamic and Lateral-Control Characteristics of a 1/28-Scale Model of the Bell X-1 Airplane Wing-Fuselage Combination: Transonic-Bump Method
Aerodynamic Characteristics at a Mach Number of 1.25 of a 6-Percent-Thick Triangular Wing and 6- and 9-Percent-Thick Triangular Wings in Combination With a Fuselage: Wing Aspect Ratio 2.31, Biconvex Airfoil Sections
Data from Tests of a 1/5-Scale Model of a Proposed High-Speed Submarine in the Langley Full-Scale Tunnel
Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction
Free-flight performance of 16-inch-diameter supersonic ram-jet units 2: five units designed for combustion-chamber-inlet Mach number of 0.16 at free-stream Mach number of 1.60 (units B-1, B-2, B-3, B-4, and B-5)
Spin Investigation of a 1/29-Scale Model of the Republic XF-91 Airplane with a Conventional Tail Installed
Investigation of a Systematic Group of NACA 1-Series Cowling With and Without Spinners
Initial Test in the Transonic Range of Four Flutter Airfoils Attached to a Freely Falling Body
A method for studying the hunting oscillations of an airplane with a simple type of automatic control
Stability of Thin-Walled Tubes Under Torsion
Characteristics of Clark Y airfoils of small aspect ratios
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