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Wind-Tunnel Investigation of the Drag and Lateral-Stability Characteristics of a 1/22-Scale Model of a Bomber Airplane Employing a Low-Aspect-Ratio Triangular Wing
Comparative Study of Turbofan and Turbojet Engines
Transonic Flutter Characteristics of a Cambered A-Plan-Form Wing With and Without Simulated Nacelles
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
Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 2 - Design and Experimental Performance of Turbine With Low-Velocity-Turning Stator and Standard Rotor
Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Wind-Tunnel Experiments Concerning the Dynamic Behavior of a Low-Speed Slowly Spinning Fin-Stabilized Rocket
Performance of Multiple Jet-Exit Installations
Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
Aerodynamic Loads on Tails at High Angles of Attack and Sideslip
Tests With Hydrogen Fuel in a Simulated Afterburner
Hydrodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane Designed for Supersonic Flight
Flutter Experiments With Various Control Configurations
Flight Test of a Solid-Fuel Ramjet With the Internal Surface of the Combustor Air Cooled
Drag at Model Trim Lift of a 1/15-Scale Convair B-58 Supersonic Bomber
The Effect of Compressor-Inlet Water Injection on Engine and Afterburner Performance
Some Research on the Lift and Stability of Wing-Body Combinations
Performance of a Short Turbojet Combustor With Hydrogen Fuel in a Quarter-Annulus Duct and Comparison With Performance in a Full-Scale Engine
An Investigation of the Effect of Target Temperature on Projectile Penetration and Cratering
Static Stability and Control of Hypersonic Gliders
Boundary-Layer-Transition Measurements in Full-Scale Flight
Calculation of External-Store Loads and Correlation With Experiment
Heat-Transfer Measurements on a Concave Hemispherical Nose Shape With Unsteady-Flow Effects at Mach Numbers of 1.98 and 4.95
Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01
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