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National Advisory Committee for Aeronautics Collection
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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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NACA Research Memorandums
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1955
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1955
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National Advisory Committee for Aeronautics Collection
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Wind-Tunnel Investigation at Low Speed of a Wing Having 63 Degree Sweepback and a Drooped Tip
Component Operating Trends During Acceleration and Deceleration of Two Hypothetical Two-Spool Turbojet Engines
An experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations
Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines
Analysis and Calculation by Integral Methods of Laminar Compressible Boundary-Layer With Heat Transfer and With and Without Pressure Gradient
Preliminary Free-Jet Performance of XRJ43-MA-3 Ram-Jet Engine at a Mach Number of 2.70
The effect of control stiffness and forward speed on the flutter of a 1/10-scale dynamic model of a two-blade jet-driven helicopter rotor
Effect of Dissociation on Thermodynamic Properties of Pure Diatomic Gases
Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures
Two Miniature Temperature Recorders for Flight Use
The compressible laminar boundary layer with heat transfer and arbitrary pressure gradient
Investigation of the Turbulent Boundary Layer on a Yawed Flat Plate
Intergranular Corrosion of High-Purity Aluminum in Hydrochloric Acid 2: Grain-Boundary Segregation of Impurity Atoms
A Self-Excited, Alternating-Current, Constant-Temperature Hot-Wire Anemometer
Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers
Variation of Local Liquid-Water Concentration About an Ellipsoid of Fineness Ratio 10 Moving in a Droplet Field
Wind-Tunnel Measurements at Subsonic Speeds of the Static and Dynamic-Rotary Stability Derivatives of a Triangular-Wing Airplane Model Having a Triangular Vertical Tail
Liquid Hydrogen as a Jet Fuel for High-Altitude Aircraft
Design and Performance of Throttle-Type Fuel Controls for Engine Dynamic Studies
Effect of Ammonia Addition on Limits of Flame Propagation for Isooctane-Air Mixtures at Reduced Pressures and Elevated Temperatures
Analytic determination of the discharge coefficients of flow nozzles
Application of the generalized shock-expansion method to inclined bodies of revolution traveling at high supersonic airspeeds
Hydrodynamic tares and interference effects for a 12-percent-thick surface-piercing strut and an aspect-ratio-0.25 lifting surface
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