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NACA Research Memorandums
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NACA Research Memorandums
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1952
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Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 3.04
Theoretical Investigation of the Effects of the Artificial-Feel System on the Maneuvering Characteristics of the F-89 Airplane
Correlation of Buffet Boundaries Predicted From Wind-Tunnel Tests With Those Measured During Flight Tests on the F8F-1 and X-1 Airplanes -Transonic-Bump Method
Investigation of an NACA 4-(5)(05)-041 Four-Blade Propeller With Several Spinners at Mach Numbers Up to 0.90
Aerodynamic Characteristics of Two Delta Wings at Mach Number 4.04 and Correlations of Lift and Minimum-Drag Data for Delta Wings at Mach Numbers From 1.62 to 6.9
The effects of tip-mounted jet nacelles on the transonic characteristics of low-aspect-ratio wings
An Investigation of the Effects of a Vortex-Generator Configuration on the Aerodynamic Characteristics of a 1/4-Scale Model of the X-1 Airplane (10-Percent-Thick Wing)
Investigation of the Aerodynamic Characteristics of the NACA RM-10 Missile (With Fins) at a Mach Number of 1.62 in the Langley 9-Inch Supersonic Tunnel
A transonic wind-tunnel investigation of the characteristics of a twisted and cambered 45 degree sweptback wing-fuselage configuration
Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap
A small-scale investigation of the effect of spanwise and chordwise positioning of an ogive-cylinder underwing nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6
Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Amplitude of Supersonic Diffuser Flow Pulsations
Preliminary Survey of Icing Conditions Measured During Routine Transcontinental Airline Operation
Correlation of predicted and experimental lateral oscillation characteristics for several airplanes
Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range
Lateral and directional dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements
The longitudinal characteristics at Mach numbers up to 0.9 of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and an aspect ratio of 10
Flight Test of a Radial-Burning Solid-Fuel Ram Jet
Investigation of Spinning and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultee XFY-1 Airplane in the Free-Spinning Tunnel, TED No. NACA DE 370
Effects of twist and camber, fences, and horizontal-tail height on the low-speed longitudinal stability characteristics of a wing-fuselage combination with a 45 degree sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)
Preliminary free-flight investigation of the zero-lift drag penalties of several missile nose shapes for infrared seeking devices
Effects of internal corner fillets on pressure recovery: Mass flow characteristics of scoop-type conical supersonic inlets
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