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Area-Suction Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 Degree Swept-Wing Airplane

Some Observations Relating to Recovery of Internal Friction During Fatigue of Aluminum

Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations

Theoretical Performance of Liquid Ammonia With Liquid Oxygen as a Rocket Propellant

Theory and Experiments on Supersonic Air-to-Air Ejectors

Turbulence and Temperature Fluctuations Behind a Heated Grid

Turbulent Shearing Stress in the Boundary Layer of Yawed Flat Plates

A Theoretical Study of Stagnation-Point Ablation

Relative Motion in the Terminal Phase of Interception of a Satellite or a Ballistic Missile

On the Statistical Theory of Turbulence

Relation of Journal Bearing Performance to Minimum Oil-Film Thickness

Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking

Turbulent Flow Through Porous Resistances Slightly Inclined to the Flow Direction

Wall Pressure Fluctuations in a Turbulent Boundary Layer

Wind-Tunnel Investigation at a Mach Number of 2.01 of Forebody Strakes for Improving Directional Stability of Supersonic Aircraft

Two-Dimensional Diffusion Theory Analysis of Reactivity Effects of a Fuel-Plate-Removal Experiment

Comparison of Performance of Two Aerodynamically Similar 14-Inch-Diameter Single-Stage Compressor Rotors of Different Chord Length

Summary of Methods of Measuring Angle of Attack on Aircraft

Stall Propagation in a Cascade of Airfoils

Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-Wing Fighter-Bomber-Type Airplane With a Top Inlet at Mach Numbers From 1.6 to 2.35

Study of Hydrogen Embrittlement of Iron by Internal-Friction Methods

Water-Impact Theory for Aircraft Equipped With Nontrimming Hydro-Skis Mounted on Shock Struts

Method of Split Rigidities and Its Application to Various Buckling Problems

Analysis of harmonic forces produced at hub by imbalances in helicopter rotor blades

Lightning Hazards to Aircraft Fuel Tanks

Low-Temperature, Vapor-Phase Oxidation of Fuel-Rich Hydrocarbon Mixtures

Data From Flow-Field Surveys Behind a Large-Scale Thin Straight Wing of Aspect Ratio 3

Flight Investigation of Effects of Retreating-Blade Stall on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Flight Investigation of Effects of Atmospheric Turbulence and Moderate Maneuvers on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Hydrodynamic Impact Loads on 30 Degree and 60 Degree V-Step Plan-Form Models With and Without Dead Rise

Free-Flight Investigation to Determine the Inlet External Drag of Four Inlet Models at Mach Numbers From 1.50 to 3.00

General Instability of Stiffened Cylinders

Hydrodynamic Impact Loads of a -20 Degree Dead-Rise Inverted-V Model and Comparisons With Loads of a Flat-Bottom Model

Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile

Induction System Characteristics and Engine Surge Occurrence for Two Fighter-Type Airplanes

The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes

Correlations Among Ice Measurements, Impingement Rates Icing Conditions, and Drag Coefficients for Unswept NACA 65A004 Airfoil

Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area

Accelerations in Transport-Airplane Crashes

Studies of OH, CO, CH, and C₂ Radiation From Laminar and Turbulent Propane-Air and Ethylene-Air Flames

Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls

Investigation of Control Signals for Variable Ramps of Twin-Duct Side Inlets

Investigation of an All-Moveable Control Surface at a Mach Number of 6.86 for Possible Flutter

A Flight Investigation of the Effects of Varied Lateral Damping on the Effectiveness of a Fighter Airplane as a Gun Platform

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers From 1.90 to 3.07

High Mach Number, Low-Cowl-Drag, External-Compression Inlet With Subsonic Dump Diffuser

Investigation of the Static Stability Characteristics of Five Hypersonic Missile Configurations at Mach Numbers From 2.29 to 4.65

Investigation of Vortex Movements About a Wing in Steady Subsonic Flow Undergoing a Large Angle-of-Attack Change in a Blast-Induced Gust

Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Simplified T-Tail Oscillating in Yaw About the Fin Midchord

Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds


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