Browse TRAIL Inventories

Investigation of the Lateral Stability Characteristics of the Douglas X-3 Configuration at Mach Numbers From 0.6 to 1.1 by Means of a Rocket-Propelled Model

Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback

Experimental Evaluation of Boron-Hydrocarbon Slurry in a 16-Inch Ram-Jet Combustor

Flow and Force Characteristics of 2-Percent-Thick Airfoils at Transonic Speeds

Initial Experiments on the Aerodynamic Cooling Associated With Large-Scale Vortical Motions in Supersonic Flow

Flight Measurements of the Transonic Drag of Models of Several Isolated External Stores and Nacelles

Flight Tests of a Delta-Wing Vertically Rising Airplane Model Powered by a Ducted Fan

Force and Pressure Measurements on Several Canopy-Fuselage Configurations at Transonic Mach Numbers 1.41 and 2.01

Flutter Experiences With Thin Pointed-Tip Wings During Flight Tests of Rocket-Propelled Models at Mach Numbers From 0.8 to 1.95

Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semicircular Air Inlet in the Root of a 45 Degree Sweptback Wing

An Investigation at Supersonic Speeds of the Effect of Varying the Maximum-Thickness Position Upon the Aerodynamic Characteristics of a Series of 3 1/2-Percent-Thick Delta Wings

Investigation of a Three-Stage Transonic Research Axial-Flow Compressor: Aerodynamic Design and Overall Performance

Investigation of a Ramp-Type Inlet Designed for Improved Angle-of-Attack Performance at Mach Number 2.0

Investigation of a High-Performance Axial-Flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area: Aerodynamic Design and Overall Performance

Standard Atmosphere - Tables and Data for Altitudes to 65,800 Feet

Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane

Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets

Failure of Materials Under Combined Repeated Stresses With Superimposed Static Stresses

Preliminary Free-Jet Performance of XRJ43-MA-3 Flight-Weight Ram-Jet Engine at Mach Numbers of 2.35, 2.50, and 2.70

Metal-Bonding Adhesives for High-Temperature Service

An accurate and rapid method for the design of supersonic nozzles

Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces

Acoustic analysis of ram-jet buzz

Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds

Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack From 0 to 90 Degrees

Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds

Amplitude of Supersonic Diffuser Flow Pulsations

An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route

An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes

Acoustical Treatment for the NACA 8- by 6-Foot Supersonic Propulsion Wind Tunnel

Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Experimental investigation of a body flare for obtaining pitch stability and a body flap for obtaining pitch control in hypersonic flight

Performance of Inconel 550 Turbine Blades in a Turbojet Engine and Effects of Different Forging Temperatures and Heat Treatments

Preliminary Investigation of a Technique of Producing a Heated Core in a Supersonic Wind-Tunnel Stream

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching From the Midsemispan and Wing-Tip Locations of a 45 Degree Sweptback Wing-Fuselage Combination

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching From the 25-Percent-Semispan and Wing-Tip Location of a 45 Degree Sweptback Wing-Fuselage Combination

An Experimental Investigation of the Flow Phenomena Over Bodies at High Angles of Attack at a Mach Number of 2.01

Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form: Longitudinal and Lateral Control Characteristics

Flight and Preflight Tests of a Ram Jet Burning Magnesium Slurry Fuel and Utilizing a Solid-Propellant Gas Generator for Fuel Expulsion

Exploratory Tests of Transpiration Cooling on a Porous 8 Degree Cone at M = 2.05 Using Nitrogen Gas, Helium Gas, and Water as the Coolants

Experimental Investigation of the Zero-Lift Wave Drag of Seven Pairs of Delta Wings With Constant and Varying Thickness Ratios at Mach Numbers of 1.62, 1.93, and 2.41

Temperature Recovery Factors on a Slender 12 Degree Cone-Cylinder at Mach Numbers From 3.0 to 6.3 and Angles of Attack Up to 45 Degrees

Some Effects of Configuration Variables on Store Loads at Supersonic Speeds

Some Effects of Fluid in Pylon-Mounted Tanks on Flutter

Some Measurements of Boiling Burn-Out

Stabilization Techniques for Ramp-Type Side Inlets at Supersonic Speeds

Preliminary Results From Flight Measurements in Gradual-Turn Maneuvers of the Wing Loads and the Distribution of Load Among the Components of a Boeing B-47A Airplane

Preliminary Results of an Investigation at Transonic Speeds to Determine the Effects of a Heated Propulsive Jet on the Drag Characteristics of a Related Series of Afterbodies

Theoretical and Experimental Investigation of the Effect of Yaw on Heat Transfer to Circular Cylinders in Hypersonic Flow

Transport of Radioactivity by Liquid Sodium in a Stainless Steel Circulation System


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