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NACA Research Memorandums
33
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NACA Research Memorandums
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1958
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1958
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Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Hydrodynamic Characteristics of Missiles Launched Under Water
Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, and 3.51
Performance of JP-4 Fuel With Fluorine-Oxygen Mixtures in 1000-Pound-Thrust Rocket Engines
Investigation of the Static Stability Characteristics of Five Hypersonic Missile Configurations at Mach Numbers From 2.29 to 4.65
Maneuver Performance of Interceptor Missiles
Effect of Dissociation on Exhaust-Nozzle Performance
An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers From 3.0 to 6.3
Canard Hinge Moments and Longitudinal Stability of a 1/7-Scale Model of the Convair B-58 External Store in a Free-Flight Investigation at Mach Numbers From 0.94 to 2.58
Effect of pressure level on afterburner-wall temperatures
Exploratory Investigation of Performance of Experimental Fuel-Rich Hydrogen Combustion System
Analytical and experimental investigation of a temperature-schedule acceleration control for a turbojet engine
A Flight-Test Study of Total-Pressure Distortion in a Thick-Lipped Nose Inlet
Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
Effect of pressure level on afterburner-wall temperatures
Effect of aerodynamic heating on the flutter of a rectangular wing at a Mach number of 2
Investigation of the Static Stability Characteristics of Five Hypersonic Missile Configurations at Mach Numbers From 2.29 to 4.65
Effect of Dissociation on Exhaust-Nozzle Performance
Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying
Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations
Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Performance of JP-4 fuel with fluorine-oxygen mixtures in 1000-pound-thrust rocket engines
Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20
Analysis of transonic rotor-blade passage loss with hot-wire anemometers
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