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NACA Research Memorandums
192
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NACA Research Memorandums
192
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1950-1959
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Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models
Analysis of Flight-Determined and Predicted Effects of Flexibility on the Steady-State Wing Loads of the B-52 Airplane
Summary and Analysis of Horizontal-Tail Contribution to Longitudinal Stability of Swept-Wing Airplanes at Low Speeds
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
Low-Speed Investigation of the Effect of Small Canard Surfaces on the Directional Stability of a Sweptback-Wing Fighter-Airplane Model
Material Compatibility With Gaseous Fluorine
Experimental Investigation of the Stability, Control, and Induced Rolling Moments of a Canard Missile Airframe at a Mach Number of 1.7
Investigation of a 1/22-Scale Model of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Lateral, Directional, and Additional Longitudinal Static Stability and Control
An Airborne Simulator Investigation of the Accuracy of an Optical Track Command Missile Guidance System
Experimental Investigation of Effect of Spike- Tip and Cowl-Lip Blunting on the Internal Performance of a Two-Cone Cylindrical-Cowl Inlet at Mach Number 4.95
Effect of Spike-Tip and Cowl-Lip Blunting on Inlet Performance of a Mach 3.0 External-Compression Inlet
Experimental Investigation of Boundary-Layer Suction Through Slots to Obtain Extensive Laminar Boundary Layers on a 15 Percent-Thick Airfoil Section at High Reynolds Numbers
Experimental Study of Isothermal Wake-Flow Characteristics of Various Flame-Holder Shapes
Some Flight Data for the Chance Vought Regulus 2 Missile
Effect of Control Trailing-Edge Thickness or Aspect Ratio on the Oscillating Hinge-Moment and Flutter Characteristics of a Flaptype Control at Transonic Speeds
Experimental Study of Ballistic-Missile Base Heating with Operating Rocket
Summary of NACA Research on Afterburners for Turbojet Engines
Investigation of Inlet Control Parameters for an External-Internal-Compression Inlet From Mach 2.1 to 3.0
Aerodynamic Loads on Tails at High Angles of Attack and Sideslip
Preliminary Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 1/20-Scale Model of the McDonnell F4H-1 Airplane at Mach Numbers of 1.59, 1.89, and 2.09
An approximate method for calculating the effect of surface roughness on the drag of an airplane
The calculation of drag for airfoil sections and bodies of revolution at subcritical speeds
Altitude-Test-Chamber Investigation of Performance of a 28-Inch Ram-Jet Engine 1: Combustion and Operational Performance of Four Combustion-Chamber Configurations
Influence of tube-entrance configuration on average heat-transfer coefficients and friction factors for air flowing in an Inconel tube
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