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Analytical Investigation of Fuel-Cooled Turbine Blades With Return-Flow Type of Finned Coolant Passages
Investigation of High-Angle-of-Attack Performance of a 14 Deg Ramp-Type Inlet in Various Circumferential Body Locations: Mach Number Range 1.5 to 2.0
Empirical Cooling Correlation for an Experimental Afterburner With an Annular Cooling Passage
Results of flight tests at supersonic speeds to determine the effect of body nose fineness ratio on body and wing drag
Numerical solution of equations for one-dimensional gas flow in rotating coolant passages
Supplementary analysis of the dynamic lateral stability characteristics of the Bell X-2 airplane as affected by variations in mass and aerodynamic parameters
An investigation of the subsonic speed range of a full-span and a semispan model of a plane wing and of a cambered and twisted wing, all having 45 degrees of sweepback
Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds
Low-Speed Characteristics of a Wing Having 63 Degrees Sweepback and Uniform Camber
Empirical cooling correlation for an experimental afterburner with an annular cooling passage
Effect of Surface Finish on Fatigue Properties at Elevated Temperatures 1: Low-Carbon N-155 With Grain Size of A.S.T.M. 1
Altitude Wind Tunnel Investigation of High-Temperature Afterburners
Experimental Investigation of Flow in the Rotating Passages of a 48-Inch Impeller at Low Tip Speeds
Effects of rate of flap deflection on flap hinge moment and wing lift through the Mach number range from 0.32 to 0.87
Turbine design considerations for turbine-propeller engine operating over a range of flight conditions
An investigation of high-frequency combustion oscillations in liquid-propellant rocket engines
A design and performance study of the nuclear direct-air-cycle supersonic airplane, including the effects of operating temperatures and fuel plate material and thickness
Effects of Compressibility at Mach Numbers Up to 0.8 on Internal-Flow Characteristics of a Cowling-Spinner Combination Equipped With an Eight-Blade Dual-Rotation Propeller
Altitude performance investigation of a high-temperature afterburner
External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers
Preliminary survey of compressor rotor-blade wakes and other flow phenomena with a hot-wire anemometer
Flight Tests of Fifteen T-231 Gun-Launched Rocket Projectiles
Effect of Ambient Conditions on the Performance of a Pressure-Jet Powerplant for a Helicopter
Injection principles for liquid oxygen and heptane using two-element injectors
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