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National Advisory Committee for Aeronautics Collection
222
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National Advisory Committee for Aeronautics Collection
222
Technical Report Archive and Image Library
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NACA Research Memorandums
181
NACA Technical Reports
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NACA Memorandum Reports
4
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3
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NACA Research Memorandums
181
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37
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1950-1959
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National Advisory Committee for Aeronautics Collection
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Drag Measurements of a 34 Degree Swept-Forward and Swept-Back NACA 65-009 Airfoil of Aspect Ratio 2.7 as Determined by Flight Tests at Supersonic Speeds
Determination of Coupled Modes and Frequencies of Swept Wings by Use of Power Series
Investigation of a Flow Deflector and an Auxiliary Scoop for Improving Off-Design Performance of Nose Inlets
Flight Test of NACA FR-1-B, a Low-Acceleration Rocket-Propelled Vehicle for Transonic Flutter Research
Preliminary Tests in the Supersonic Sphere
Results of measurements of maximum lift and buffeting intensities obtained during flight investigation of the Northrop X-4 research airplane
Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range From 0.5 to 0.95
Flight data pertinent to buffeting and maximum normal-force coefficient of the Douglas X-3 research airplane
Estimation of F-3 and F-4 knock-limited performance ratings for ternary and quaternary blends containing triptane or other high-antiknock aviation-fuel blending agents
A Simplified Method of Elastic-Stability Analysis for Thin Cylindrical Shells
Critical Stress of Thin-Walled Cylinders in Axial Compression
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds
Heat Transfer and Pressure Distribution at a Mach Number of 6.8 on Bodies With Conical Flares and Extensive Flow Separation
Performance of J33-A-23 Turbojet-Engine Compressor, Part 1, Over-All Performance Characteristics of Compressor with 17-Blade Impeller
Performance of Variable Two-Dimensional Inlet Designed for Engine-Inlet Matching 1 - Performance at Design Mach Number of 3.07
Effects of Rocket-Armament Exhaust Gas on the Performance of a Supersonic-Inlet J34-Turbojet-Engine Installation at Mach 2.0
Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double-Wedge Sections With the Maximum Thickness at 0.18 Chord
Flight and Test-Stand Investigation of High-Performance Fuels in Double-Row Radial Air-Cooled Engines 1: Determination of Cooling Characteristics of Flight Engine
Tank investigation of the hydrodynamic characteristics of a 1/3.33-scale jet-powered dynamic model of the Martin XP6M-1 flying boat with a revised forebody planing bottom : TED No. NACA DE 385
Total-Pressure and Schlieren Studies of the Wakes of Various Canard Control Surfaces Mounted on a Missile Body at a Mach Number of 1.93
The low-speed lift and pitching moment characteristics of a 45 degree sweptback wing of aspect ratio 8 with and without high-lift and stall-control devices as determined from pressure distribution at a Reynolds number of 4.0 x 10(exp 6)
Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor
Performance of Pentaborane, Pentaborane - JP-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-scale Turbojet Engine
Performance of Pentaborane, Pentaborane - JP-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-Scale Turbojet Engine
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