Browse TRAIL Inventories

An Investigation of Ejection Releases of Submerged and Semisubmerged Dynamically Scaled Stores From a Simulated Bomb Bay of a Fighter-Bomber Airplane at Supersonic Speeds

Investigation of Ejection Release Characteristics of Four Dynamically Scaled Internal-Store Shapes From a 1/17-Scale Simulated Bomb Bay of the Republic F-105 Airplane at Mach Numbers of 1.39 and 1.98

Tabulated Pressure Data for a Series of Controls on a 60 Degree Delta Wing at Mach Numbers of 1.61 and 2.01

Investigation of Afterburner Combustion Screech and Methods of Its Control at High Combustor Pressure Levels

Attenuation of Tangential-Pressure Oscillations in a Liquid-Oxygen-n-Heptane Rocket Engine With Longitudinal Fins

Simulated Flight Investigation of Scaled-Speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip

Some Design and Operational Considerations of a Liquid-Hydrogen Fuel and Heat-Sink System for Turbojet-Engine Tests

Some Interference Effects That Influence Vertical-Tail Loads at Supersonic Speeds

Static Lateral-Directional Stability Characteristics of Five Contemporary Airplane Models From Wind-Tunnel Tests at High Subsonic and Supersonic Speeds

Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles

Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages

A Summary of Results Obtained During Flight Simulation of Several Aircraft Prototypes With Variable-Stability Airplanes

Summary of Subsonic-Diffuser Data

Full-Scale Wind-Tunnel Tests of a North American FJ-3 Airplane with a Spoiler-Slot-Deflector Lateral Control System

Flight Test of a Solid-Fuel Ramjet With the Internal Surface of the Combustor Air Cooled

Flutter Tests of a 1/25-Scale Model of the B-36J/RF-84F Tip-Coupled Airplane Configuration in the Langley 19-Foot Pressure Tunnel

Investigation of a 1/22-Scale of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Static Longitudinal Stability and Control and Performance Characteristics at Transonic Speeds

Annual Report of the National Advisory Committee for Aeronautics (42nd): Administrative Report without Technical Reports

Aerodynamic Principles for the Design of Jet-Engine Induction Systems

Aerodynamics of Missiles Employing Wings of Very Low Aspect Ratio

Free-flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Deg Sweptback Wing of Aspect Ratio 4

Turbine Failure Investigation of J65-W-4 Turbojet Engine in an Altitude Test Chamber

An Analytic Study of Turbojet Engine Thrust Augmentation With Liquid Hydrogen, Pentaborane, Magnesium Slurry, and JP-4 Afterburner Fuels and a 220-Second Impulse Rocket

Chemical and Physical Properties of a Boron-Carbon-Hydrogen Fuel Z-244 (NACA 55Z8)

A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift

Spontaneous Ignition Studies Relating to Lubricants of Reduced Flammability

Design Criteria for Axisymmetric and Two-Dimensional Supersonic Inlets and Exits

Correlation of Crippling Strength of Plate Structures With Material Properties

Correlation of Supersonic Convective Heat-Transfer Coefficients From Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)

Boundary-Layer Growth and Shock Attenuation in a Shock Tube With Roughness

Investigation of Suction Slot Shapes for Controlling a Turbulent Boundary Layer

Investigation of the Effect of Impact Damage on Fatigue Strength of Jet-Engine Compressor Rotor Blades

Investigation of Far Noise Field of Jets 2: Comparison of Air Jets and Jet Engines

Investigation of the Use of the Thermal Decomposition of Nitrous Oxide to Produce Hypersonic Flow of a Gas Closely Resembling Air

Tabulated Pressure Coefficient Data from a Tail Loads Investigation on a 1/15-Scale Model of the Goodyear XZP5K Airship

Preliminary Internal Performance Data for a Variable-Ejector Assembly on the XJ79-GE-1 Turbojet Engine 1: Nonafterburning Configurations

On Landing Gear Stresses

Static Longitudinal Stability Characteristics of a Series of 90-Millimeter Artillery Shells at Mach Numbers of 0.8, 0.9, 1.0, and 1.2

Wind-Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Degree Swept-Wing Airplane

On the Theory of Thin Shallow Shells

On the Calculation of Shallow Shells

On the Theory of Anisotropic Shallow Shells

Annual Report of the National Advisory Committee for Aeronautics (40th). Administrative Report Including Technical Report Nos. 1158-1209

Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104A Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. AF-245

Component Performance Investigation of J71 Experimental Turbine 2 - Internal-Flow Conditions with 97-Percent-Design Stator Areas

Component Performance Investigation of J71 Experimental Turbine 4 - Effect of First-Stator Adjustment; Over-All Performance of J71-97 Turbine With 132-Percent-Design Stator Area

Component Performance Investigation of J71 Experimental Turbine 3 - Effect of Third-Stage Shrouding on Over-All Performance

Aeroelastic Problems of Airplane Design

Altitude Acceleration Investigation of the RA-14 Avon Turbojet Engine

Flight Investigation to Determine the Effect of Jet Exhaust on Drag, Trim Characteristics, and Afterbody Pressures of a 0.125-Scale Rocket Model of the McDonnell F-101A Airplane


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