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Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for the B-26 Airplane

Author: Langley Aeronautical Laboratory

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Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-speed Missiles

Author: Langley Aeronautical Laboratory

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Resistance Tests of Models of Three Flying-boat Hulls With a Length-beam Ration of 10.5

Author: Langley Aeronautical Laboratory

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Flight Investigation of Boundary-layer Transition and Profile Drag of an Experimental Low-drag Wing Installed on a Fighter-type Airplane

Author: Langley Aeronautical Laboratory

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Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface

Author: Langley Aeronautical Laboratory

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Flow of Gas Through Turbine Lattices

Author: Langley Aeronautical Laboratory

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Stresses Around Rectangular Cut-outs in Skin-stringer Panels Under Axial Loads - II

Author: Langley Aeronautical Laboratory

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Determination of Induced Velocity in Front of an Inclined Propeller by a Magnetic-analogy Method

Author: Langley Aeronautical Laboratory

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Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-flight Tunnel

Author: Langley Aeronautical Laboratory

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Wind-tunnel Investigation of a Rectangular NACA 2212 Airfoil With Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aerodynamic Brakes

Author: Langley Aeronautical Laboratory

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Effects of Wing and Nacelle Modifications on Drag and Wake Characteristics of a Bomber-type Airplane Model

Author: Langley Aeronautical Laboratory

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Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports

Author: Langley Aeronautical Laboratory

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Comparison of Yaw Characteristics of a Single-engine Airplane Model With Single-rotating and Dual-rotating Propellers

Author: Langley Aeronautical Laboratory

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Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic Characteristics of a Full-scale Horizontal Tail Surface

Author: Langley Aeronautical Laboratory

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Charts for the Minimum-weight Design of 24S-T Aluminum-alloy Flat Compression Panels With Longitudinal Z-section Stiffeners

Author: Langley Aeronautical Laboratory

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Effect of Normal Pressure on the Critical Shear Stress of Curved Sheet

Author: Langley Aeronautical Laboratory

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Flight Investigation at High Speeds of Flow Conditions Over an Airplane Wing as Indicated by Surface Tufts

Author: Langley Aeronautical Laboratory

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Effect of Compressibility on the Hovering Performance of Two 10-foot-diameter Helicopter Rotors Tested in the Langley Full-scale Tunnel

Author: Langley Aeronautical Laboratory

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Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered With Camouflage Paint

Author: Langley Aeronautical Laboratory

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Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 2.04

Author: Langley Aeronautical Laboratory

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