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Full-Scale Evaluation of Some Flameholder Design Concepts for High-Inlet-Velocity Afterburners

The Origin and Distribution of Supsonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5 - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number, 2.01

The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselagestore Configurations 6. - Swept-Wing Heavy-Bomber Configuration With Stores of Different Sizes and Shapes

Low-Speed Roll Effectiveness of a Differentially Deflected Horizontal-Tail Surface on a 42 Degree Swept-Wing Model

Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71

Performance at Simulated High Altitudes of a Prevaporizing Annular Turbojet Combustor Having Low Pressure Loss

Performance of a Short Turbojet Combustor With Hydrogen Fuel in a Quarter-Annulus Duct and Comparison With Performance in a Full-Scale Engine

Transonic Aerodynamic and Trim Characteristics of a Multi-Engine Delta-Wing Airplane Model

Compilation and Analysis of U.S. Turbojet and Ram-Jet Engine Characteristics

Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96

Aerodynamic Loads on an External Store Adjacent to a 60 Degree Delta Wing at Mach Numbers From 0.75 to 1.96

Afterburner Performance With Combustion-Chamber Lengths From 10 to 62 Inches at Several Afterburner-Inlet Temperatures

Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds

The Appearance of a Boric Oxide Exhaust Cloud From a Turbojet Engine Operating on Trimethylborate Fuel

Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a 1/15-Scale Model of the Grumman F11F-1F Airplane at Mach Numbers of 1.56, 1.76, 2.06, and 2.53

Longitudinal Aerodynamic Characteristics of Various Configurations of a Revised 1/22-Scale Model of the Republic F-105 Airplane at Mach Numbers of 1.41 and 2.01

An Investigation of the Afterbody Pressure Distribution and Fin Loading Characteristics of a Specialized Store Configuration at Transonic Speeds

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


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