Langley Aeronautical Laboratory
Bibliografía (100 obras)
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating near the Free Water Surface
2023
Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds
2023
Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed Missiles
2021
Flight Investigation of NACA Aileron Modifications for the Improvement of the Lateral Control Characterisitcs of a High-Speed Fighter Airplance
2021
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight Tunnel
2021
Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint
2021
Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2. 05, 2. 54, And 2. 04
2021
Heat Transfer and Pressure Measurement on a 5-Inch Hemispherical Concave Nose at a Mach Number Of 2. 0
2021
Correlation of Supersonic Convective Heat-Transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
2021
Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients
2021
Flight Studies of the Horizontal-Tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers
2021
Investigation of Methods of Supporting Single-Thickness Specimens in a Fixture for Determination of Compressive Stress-strain Curves
2021
Effect of Compressibility on the Pressures and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0. 20-Chord Flap
2021
Wind-Tunnel Investigation of a Rectangular NACA 2212 Airfoil with Semispan Ailerons and with Nonperforated, Balanced Double Split Flaps for Use As Aerodynamic Brakes
2021
Wind-Tunnel Investigation of an NACA 23021 Airfoil with a 0. 32-airfoil-chord Double Slotted Flap
2021
Free-Flight Measurements of Aerodynamic Heat Transfer to Mach Number 3. 9 and of Drag to Mach Number 6. 9 of a Fin-stabilized Cone-cylinder Configuration
2021
Lifting-Surface-theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces
2021
Airfoil-Contour Modifications Based on [epsilon]-curve Method of Calculating Pressure Distribution
2021
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating near the Free Water Surface
2021
Flight Investigation at High Speeds of Flow Conditions over an Airplane Wing As Indicated by Surface Tufts
2021
Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds
2021
Effects of Roughness at High Reynolds Numbers on the Lift and Drag Characteristics of Three Thick Airfoils
2021
Determination of the Stability and Control Characteristics of a Straight-Wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel
2021
Effect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 Airplane
2021
Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag
2021
Influence of Vertical-Tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model with One Engine Inoperative
2021
Determination of the Effect of Horizontal-Tail Flexibility on Longitudinal Control Characteristics
2021
Conformal Transformation of an Airfoil into a Straight Line and Its Application to the Inverse Problem of Airfoil Theory
2021
Wind-Tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane
2021
Flight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-drag Wing Installed on a Fighter-type Airplane
2021
Method for Studying the Hunting Oscillations of an Airplane with a Simple Type of Automatic Control
2021
Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-Section Stiffeners
2021
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
2021
Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped with Spring-Tab Ailerons
2021
Wind-Tunnel Tests of a Blunt-nose Aileron with Beveled Trailing Edge on an NACA 66(215)-216 Airfoil with Several Modifications of Aileron Nose and Adjacent Airfoil Contour
2021
Flow Past a Straight- and a Swept-Wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1. 0
2021
Approximate Determination of the Power Required to Move Control Surfaces As Related to Control-Booster Design
2021
Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes
2021
Column and Plate Compressive Strengths of Aircraft Structural Materials Extruded 75S-T Aluminum-Alloy
2021
Numerical Evaluation of the Wake-Survey Equations for Subsonic Flow Including the Effect of Energy Addition
2021
Effect of Compressibility on the Hovering Performance of Two 10-Foot-diameter Helicopter Rotors Tested in the Langley Full-scale Tunnel
2021
Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous over Three Supports
2021
Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas a-26 Airplane
2021
Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot-span Fighter-type Wing of NACA 230-series Airfoil Sections
2021
Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04
1952
Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls
1945
Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high mach numbers
1945
Flight investigation of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane
1945
Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance
1945
Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane
1945
Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils from Tests in the NACA Two-Dimensional Low-turbulence Pressure Tunnel
1944
Scale and turbulence effects on the lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section
1944
Scale-effect tests in a turbulent tunnel of the NACA 653-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap
1944
On the flow of a compressible fluid by the hodograph method. I- Unification and extension of present-day results
1944
Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnel
1944