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Wind-Tunnel Experiments Concerning the Dynamic Behavior of a Low-Speed Slowly Spinning Fin-Stabilized Rocket

Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/10-Scale Model of the Douglas A4D-1 Airplane

Wind-Tunnel Investigation at Low Speed of the Yawing Stability Derivatives of a 1/10-Scale Model of the Douglas A4D-1 Airplane

Design of Combustor for Long-Range Ram-Jet Engine and Performance of Rectangular Analog

Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models

Experimental Determination of Thermal Conductivity of Low-Density Ice

The Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Lateral Stability Characteristics of a 1/6- Scale of the MX-1764 Airplane

Effects of Secondary-Air Flow on Annular Base Force of a Supersonic Airplane

Performance of Isentropic Nose Inlets at Mach Number of 5.6

Combustion Performance of Two Experimental Turbojet Annular Combustors at Conditions Simulating High-Altitude Supersonic Flight

Comparison of Free-Flight Measurements of the Zero-Lift Drag Rise of Six Airplane Configurations and Their Equivalent Bodies of Revolution at Transonic Speeds

Comparison of Wind-Tunnel, Rocket, and Flight Drag Measurements for Eight Airplane Configurations at Mach Numbers Between 0.7 and 1.6

Altitude Investigation of Can-Type Flame Holder in 20-Inchdiameter Ram-Jet Combustor

Investigation of Adjustable Supersonic Inlet in Combination With J34 Engine Up to Mach 2.0

Flight Investigation to Evaluate the Roll-Rate Stabilization System of the Naval Ordnance Test Station SIDEWINDER Missile at Mach Numbers From 0.9 to 2.3

Investigation of Effect of Number and Width of Annular Flameholder Gutters on Afterburner Performance

An Investigation of the Longitudinal Stability and Afterbody Pressure Characteristics of Specialized Store Configurations at Transonic Speeds

Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Longitudinal Stability Characteristics and Quantity Flow of a 1/6-Scale Model of the MX-1764 Airplane

Influence of Combustion-chamber Length on Afterburner Performance

Impingement of Water Droplets on NACA 65A004 Airfoil at 8 Degree Angle of Attack

Impingement of Water Droplets on an Ellipsoid with Fineness Ratio 5 in Axisymmetric Flow

Free-Flight Investigation of the Full-Scale Hughes Falcon Missile, D Configuration, to Determine Aileron Effectiveness and Damping in Roll

Free-flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds

Flight Test of an End-Burning Solid-Fuel Ramjet

Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Influence of Trailing-Edge Flap Span and Deflection on the Longitudinal Characteristics

Cooling Characteristics of a Transpiration-Cooled Afterburner With a Porous Wall of Brazed and Rolled Wire Cloth

A Nonlinear Theory of Bending and Buckling of Thin Elastic Shallow Spherical Shells

An Exploratory Investigation of Some Types of Aeroelastic Instability of Open and Closed Bodies of Revolution Mounted on Slender Struts

A System for Measuring the Dynamic Lateral Stability Derivatives in High-Speed Wind Tunnels

Some Measurements of Noise From Three Solid-Fuel Rocket Engines

Turbulent-Heat-Transfer Measurements at a Mach Number of 3.03

Theoretical Investigation at Subsonic Speeds of the Flow Ahead of a Slender Inclined Parabolic-Arc Body of Revolution and Correlation With Experimental Data Obtained at Low Speeds

Elastic Buckling Under Combined Stresses of Flat Plates With Integral Waffle-Like Stiffening

Burning Times of Magnesium Ribbons in Various Atmospheres

Investigation of Lift, Drag, and Pitching Moment of a 60 Degrees Delta-Wind-Body Combination (AGARD Calibration Model B) in the Langley 9-Inch Supersonic Tunnel

Lubricants of Reduced Flammability

An Investigation of the Creep Lifetime of 75S-T6 Aluminum-Alloy Columns

Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3

Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers

The Free-Stream Boundaries of Turbulent Flows

Experimental investigation of notch-size effects on rotating-beam fatigue behavior of 75S-T6 aluminum alloy

Influence of Exposed Area on Stress-Corrosion Cracking of 24S Aluminum Alloy

Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Longitudinal Stability and Control

Vertical Descent and Landing Tests of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane in Still Air, TED No. NACA DE 368

Preliminary Altitude Performance Data for the J65-B3 Turbojet Engine at Reynolds Number Indices from 0.2 to 0.8

Performance and Boundary-Layer Data From 12 Degree and 23 Degree Conical Diffusers of Area Ratio 2.0 at Mach Numbers Up to Choking and Reynolds Numbers Up to 7.5 X 10(6)

Performance of Air-Launched T-40 Rocket Motors with Two Types of Igniter

Experiments on a Tail-Wheel Shimmy

Static Longitudinal and Lateral Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane at a Mach Number of 1.41

Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds


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