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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Wind-Tunnel Investigation at Low Speed of Sideslipping, Rolling, Yawing, and Pitching Characteristics for a Model of a 45 Degree Swept-Wing Fighter-Type Airplane
Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages 6: over-all performance, rotating stall, and blade vibration at low and intermediate compressor speeds
Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Complete Model With an Unswept Wing and a Sweptback Horizontal Tail at Two Vertical Locations
Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory
Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips
Comparative Dispersion Data From Ground-Launched 2.25-Inch Rockets Equipped With Cruciform and Monoplane Fins
Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory
A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound
Comparative Tests of the Strength and Tightness of Commercial Flush Rivets of One Type and NACA Flush Rivets in Machine-Countersunk and Counterpunched Joints
Low-Speed Wind-Tunnel Tests of a 1/8-Scale Model of the Bell D-188A VTOL Airplane
Effect of Reduced Stator-Blade Trailing-Edge Thickness on Over-All Performance of a Transonic Turbine
Investigation of Power Requirements for Ice Prevention and Cyclical De-Icing of Inlet Guide Vanes with Internal Electric Heaters
An Investigation of the Afterbody Pressure Distribution and Fin Loading Characteristics of a Specialized Store Configuration at Transonic Speeds
Survey of Supersonic Inlets for High Mach Number Applications
Performance of Several Half-Conical Side Inlets at Supersonic and Subsonic Speeds
Afterburner Performance With Combustion-Chamber Lengths From 10 to 62 Inches at Several Afterburner-Inlet Temperatures
A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390
Wind-Tunnel Measurement of Static Forces on Internally Carried Bombs of Two Different Bluff Shapes in the Flow Field of a Swept-Wing Fighter-Bomber Configuration at a Mach Number of 1.6
A Comparison of the Maneuvering Performance of a Monowing Versus a Cruciform Missile
First Landing of Bell X-2 Research Airplane
NACA Conference on Aerodynamics of High Speed Aircraft
Fuel investigation in a tubular-type combustor of a turbojet engine
An empirically derived method for calculating pressure distribution at supercritical Mach numbers and moderate angles of attack
Pressure recovery at supersonic speeds through annular duct inlets situated in a region of appreciable boundary layer 1: addition of energy to the boundary layer
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