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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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NACA Research Memorandums
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1951
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1951
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National Advisory Committee for Aeronautics Collection
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1951
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Damping in Roll of Rocket-Powered Test Vehicles Having Swept, Tapered Wings of Low Aspect Ratio
Estimated deceleration of airplane nose section jettisoned at various altitudes and airspeeds
Longitudinal-control effectiveness and downwash characteristics at a Mach number of 1.24 of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method
The Preparation, Physical Properties, and Heats of Combustion of Four Alkylsilanes
Sound from a two-blade propeller at supersonic tip speeds
Derivation of the Equations of Motion of a Symmetrical Wing-Tip-Coupled Airplane Configuration With Rotational Freedom at the Junctures
Preliminary Experimental Investigation of Flutter Characteristics of M and W Wings
Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 4 with 3-percent-thick, biconvex section
Free-flight measurements at Mach numbers from 0.7 to 1.6 of some effects of airfoil-thickness distribution and trailing-edge angle on aileron rolling effectiveness and drag for wings with 0 and 45 degrees sweepback
Some Effects of Fuselage Interference, Wing Interference, and Sweepback on the Damping in Roll of Untapered Wings as Determined by Techniques Employing Rocket-Propelled Vehicles
An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils
Flying qualities of a high-performance personal-owner airplane
Factors Affecting the Starting Characteristics of Gas-Turbine Engines
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