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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398
Flight determination of minimum drag of 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with modified fuselage area distribution and faired inlet at Mach number from 0.82 to 1.68 : TED No. NACA DE 392
Application of area suction to leading-edge and trailing-edge flaps on a 44 degree swept-wing model
Analysis of some parameters used in correlating blowing-type boundary-layer control data
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds
Measurements of Boundary-Layer Transition at Low Speed on Two Bodies of Revolution in a Low-Turbulence Wind Tunnel
Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0
Transonic Flight Evaluation of the Effects of Fuselage Extension and Indentation on the Drag of a 60 Degree Delta-Wing Interceptor Airplane
An Investigation of Screens for Removing Distortions in Ducted Flows at High Subsonic Speeds
Investigation at transonic speeds of loading over a 30 degree sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on a body
Flight Investigation of the Low-Speed Characteristics of a 35 Degree Swept-Wing Airplane Equipped with an Area-Suction Ejector Flap and Various Wing Leading-Edge Devices
Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5
Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices
Resistance of Various Materials to Attack by Molten Bismuth-Lead Eutectic at Elevated Temperatures
Wind-tunnel investigation of a wing-root inlet configuration with various modifications at Mach numbers of 1.41, 1.81, and 2.01
The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders
The drag of two streamline bodies as affected by protuberances and appendages
Supersonic Flow Around Circular Cones at Angles of Attack
Investigation of Air Flow in Open-Throat Wind Tunnels
Convection of a pattern of vorticity through a shock wave
Wind-Tunnel Tests to Determine Aileron Characteristics of the McDonnell XFD-1 Airplane, TED No. NACA 23102
Effects of systematic changes of trailing-edge angle and leading-edge radius on the variation with Mach number of the aerodynamic characteristics of a 10-percent-chord-thick NACA airfoil section
Measurement of distortion in second experimental control rod with temperature patterns simulating shim rod out and shim rod 50 percent inserted for Argonne Naval Reactor
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