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National Advisory Committee for Aeronautics Collection
239
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National Advisory Committee for Aeronautics Collection
239
Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Research Memorandums
211
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1950-1959
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National Advisory Committee for Aeronautics Collection
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Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 1: effect of air bleed at compressor outlet
Additional Fatigue Tests on Effects of Design Details in 355-T6 Sand-Cast Aluminum Alloy
Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds
Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-Chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees
Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch
Aerodynamic characteristics of a full-span trailing-edge control on a 60 degree delta wing with and without a spoiler at Mach number 1.61
Aerodynamic Characteristics of Flying-Boat Hulls Having Length-Beam Ratios of 20 and 30
An Air-Borne Target Simulator for Use With Scope-Presentation Type Fire-Control Systems
An air-flow-direction pickup suitable for telemetering use on pilotless aircraft
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 3 - 18.00-Inch-Diameter Jet Nozzle
Altitude Component Performance of the YJ73-GE-3 Turbojet Engine
Altitude investigation of three flame-holder and fuel-systems configurations in a short converging afterburner on a turbojet engine
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, 7, Pressure and Temperature Distributions
Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine
Analysis of 2-Spar Cantilever Wings With Special Reference to Torsion and Load Transference
Analysis of a flight investigation at supersonic speeds of a simple homing system
An Analysis of Airspeeds and Mach Numbers Attained by Lockheed Constellation Airplanes in Transcontinental Operations During the Early Summer of 1946
Analysis of parameters for thrust control of a turbojet engine equipped with air-inlet throttle and variable-area exhaust nozzle
Analysis of the dynamic lateral stability characteristics of the Bell X-2 airplane as affected by variations in mass, aerodynamic, and dimensional parameters
An Analysis of the Effect of Structural Feedback on the Flutter of a Control Surface Having a Power-Boost System
Analytical Comparison of a Standard Turbojet Engine, a Turbojet Engine with a Tail-Pipe Burner, and a Ram-Jet Engine
Analytical determination of local surface heat-transfer coefficients for cooled turbine blades from measured metal temperatures
The Appearance of a Boric Oxide Exhaust Cloud From a Turbojet Engine Operating on Trimethylborate Fuel
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