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An Investigation of the Longitudinal Characteristics of the X-3 Configuration Using Rocket-Propelled Models: Preliminary Results at Mach Numbers From 0.65 to 1.25

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Low-Speed Stalling and Lift Characteristics

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of the Buffet Boundary and Peak Airplane Normal-Force Coefficients at Mach Numbers Up to 0.90

Flight Tests at Supersonic Speeds to Determine the Effect of Taper on the Zero-Lift Drag of Sweptback Low-Aspect-Ratio Wings

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers Up to 0.87

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of Wing Loads at Mach Numbers Up to 0.87

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Lateral Control Characteristics as Measured in Abrupt Aileron Rolls at Mach Numbers Up to 0.86

Flight Measurements of the Pressure Distribution on the Wing of the X-1 Airplane (10 Percent Thick Wing) Over a Chordwise Station Near the Midspan, in Level Flight at Mach Numbers From 0.79 to 1.00 and in a Pull Up at a Mach Number of 0.98

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: Static Lateral Control Characteristics at Mach Numbers of 1.40 and 1.59

Investigation of a Shrouded and an Unshrouded Axial-Flow Supersonic Compressor

Investigation at Mach Number 1.62 of the Pressure Distribution Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap

Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-Edge Thickness on the Aileron Hinge-Moment and Flutter Characteristics at Transonic Speeds

Experimental Investigation of Spreading Characteristics of Choked Jets Expanding into Quiescent Air

Rough-Water Tests of Models of the Vosper and Plum Planing Boats

Preliminary Results From Fatigue Tests With Reference to Operational Statistics

Equations of Motion of a Rocket

Two-Dimensional Symmetrical Inlets With External Compression

Range Performance of Bombers Powered by Turbine-Propeller Power Plants

Time Histories of Horizontal-Tail Loads, Elevator Loads, and Deformations on a Jet-Powered Bomber Airplane During Abrupt Pitching Maneuvers at Approximately 20,000 Feet

Vibration of a Wing of Finite Span in a Supersonic Flow

Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds: Several Combinations of the Tail With Each of Two Foreshortened Body Segments

A Wind-Tunnel Investigation of the Effects of Thrust-Axis Inclination on Propeller First-Order Vibration

Investigation of the Model Me 210 in the Spin Wind Tunnel of the DVL: Fourth Partial Report - Model With Long Fuselage and With a Vee Tail

The Zero-Lift Drag of Several Configurations of the XAAM-N-2 Pilotless Aircraft, TED No. NACA DE332

Tests of a Hermes A-2 Missile Body at Mach Number 4.04

Preliminary Results Obtained from Flight Test of a Rocket Model Having the Tail Only of the Grumman XF10F Airplane Configuration, TED No. NACA DE 354

Summary of Investigations of Mark 25 Aerial-Torpedo Turbine

Subsonic Gas Flow Past A Wing Profile

Exact Solutions of Equations of Gas Dynamics

The External-Shock Drag of Supersonic Inlets Having Subsonic Entrance Flow

Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction

Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed

Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed

Dependence of the Elastic Strain Coefficient of Copper on the Pre-Treatment

The Development of a Hollow Blade for Exhaust Gas Turbines

General Solution of Prandtl's Boundary-Layer Equation

Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line

Effect of Intense Sound Waves on a Stationary Gas Flame

Theory of Plane, Symmetrical Intake Diffusers

Turbulence and Heat Stratification

The Solution of the Laminar-Boundary-Layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration

The Stability of the Compression Cover of Box Beams Stiffened by Posts

Contribution to the Problem of Buckling of Orthotropic Plates, With Special Reference to Plywood

Some Effects of Nonlinear Variation in the Directional-Stability and Damping-in-Yawing Derivatives on the Lateral Stability of an Airplane

Analysis of Turbulent Free-Convection Boundary Layer on Flat Plate

The Diffusion of a Hot Air Jet in Air in Motion Part 2: The Flow Field in the Transition Zone

Graphical Determination of Wall Temperatures for Heat Transfers Through Walls of Arbitrary Shape

Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41

Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers with Zero Pressure Gradient

Small Bending and Stretching of Sandwich-Type Shells


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