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National Advisory Committee for Aeronautics Collection
214
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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NACA Research Memorandums
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Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections
The Aerodynamic Characteristics of Airfoils at Negative Angles of Attack
Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01
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
Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Characteristics at a Mach number of 1.53 including effect of small variations of sweep
Air-flow characteristics of brazed and rolled wire filter cloth for transpiration-cooled afterburners
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle
Altitude performance investigation of a high-temperature afterburner
Altitude Wind Tunnel Investigation of High-Temperature Afterburners
Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loading 2 - Curtiss 838-1C2-18R1 Four-Blade Propeller
Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 4 - Curtiss 732-1C2-0 Four-Blade Propeller
Analysis of effect of basic design variables on subsonic axial-flow-compressor performance
Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
Analysis of some parameters used in correlating blowing-type boundary-layer control data
Analysis of the turbojet engine for propulsion of supersonic fighter airplanes
Analytical Investigation of Fuel-Cooled Turbine Blades With Return-Flow Type of Finned Coolant Passages
Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages
Application of area suction to leading-edge and trailing-edge flaps on a 44 degree swept-wing model
Application of Theodorsen's Theory to Propeller Design
Arrangements of jet engine and airframe for increased range
Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers
Calculated Performance of a Mercury-Compressor-Jet Powered Airplane Using a Nuclear Reactor as an Energy Source
Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts
Combustion Performance of Two Experimental Turbojet Annular Combustors at Conditions Simulating High-Altitude Supersonic Flight
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