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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
24
Technical Report Archive and Image Library
24
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NACA Research Memorandums
16
NACA Technical Reports
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NACA Research Memorandums
16
NACA Technical Reports
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1950-1959
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1930-1939
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April
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National Advisory Committee for Aeronautics Collection
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Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane
Effect of a pilot's canopy on the drag of an NACA RM-2 drag research model in flight at transonic and supersonic speeds
Effects of high-lift and stall-control devices, fuselage, and horizontal tail on a wing swept back 42 degrees at the leading edge and having symmetrical circular-arc airfoils sections at a Reynolds number of 6.9 x 10(exp 6)
Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc section and 40 degree sweepback: a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.40
Review of Current and Anticipated Lubricant Problems in Turbojet Engines
Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54
Review of Flight Tests of NACA C and D Cowlings on the XP-42 Airplane
A Wind-Tunnel Investigation of the Effects of Thrust-Axis Inclination on Propeller First-Order Vibration
Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
Effect of Mach Number on Boundary-Layer Transition in the Presence of Pressure Rise and Surface Roughness on an Ogive-Cylinder Body with Cold Wall Conditions
The Effects Upon Body Drag of Jets Exhausting From Wing-Mounted Nacelles
Investigation of the effects of body camber and body indentation on the longitudinal characteristics of a 60 degree delta-wing-body combination at a Mach number of 1.61
Maximum Altitude and Maximum Mach Number Obtained With the Modified Douglas D-558-II Research Airplane During Demonstration Flights
Two Experiments on Applications of the Transonic Area Rule to Asymmetric Configurations
Effect of Various Modifications on Drag and Longitudinal Stability and Control Characteristics at Transonic Speeds of a Model of the XF7U-1 Tailless Airplane: NACA Wing-FLow Method, TED No. NACA DE 307
Resume and analysis of NACA lateral control research
Approximate Stress Analysis of Multistringer Beams With Shear Deformation of the Flanges
The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data
Interference on an Airfoil of Finite Span in an Open Wind Tunnel
Tests of nacelle-propeller combinations in various positions with reference to wings 3: Clark y wing - various radial-engine cowlings - tractor propeller
Performance of 15-Stage Experimental J71 Axial-Flow Compressor. 3 - Effects of Inlet-Guide-Vane Adjustment
Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects
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