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NACA Technical Reports
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Icing-Protection Requirements for Reciprocating-Engine Induction Systems
Blockage Corrections for Three-Dimensional-Flow Closed-Throat Wind Tunnels, with Consideration of the Effect of Compressibility
The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections
Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment
Elastic and plastic buckling of simply supported solid-core sandwich plates in compression
Determination of plate compressive strengths at elevated temperatures
The Aerodynamic Forces on Slender Plane- and Cruciform-Wing and Body Combinations
Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow
Comparison between theory and experiment for wings at supersonic speeds
On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid
Equations and Charts for the Rapid Estimation of Hinge-Moment and Effectiveness Parameters for Trailing-Edge Controls Having Leading and Trailing Edges Swept Ahead of the Mach Lines
Some Effects of Nonlinear Variation in the Directional-Stability and Damping-in-Yawing Derivatives on the Lateral Stability of an Airplane
The Stability of the Compression Cover of Box Beams Stiffened by Posts
Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces
Analysis of temperature distribution in liquid-cooled turbine blades
Automatic control systems satisfying certain general criterions on transient behavior
Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers with Zero Pressure Gradient
Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data
Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data
Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
Inelastic Column Behavior
Effect on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system
Two-and Three-Dimensional Unsteady Lift Problems in High-Speed Flight
Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
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