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NACA Technical Notes
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An Analysis of Ramjet Engines Using Supersonic Combustion
Analysis of the Creep Behavior of a Square Plate Loaded in Edge Compression
Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages
Analytical and Experimental Investigation of Temperature Recovery Factors for Fully Developed Flow of Air in a Tube
An analytical study of turbulent and molecular mixing in rocket combustion
An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations
Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll
Approximate Method for Calculation of Laminar Boundary Layer With Heat Transfer on a Cone at Large Angle of Attack in Supersonic Flow
Approximate solutions of a class of similarity equations for three-dimensional, laminar, incompressible boundary-layer flows
Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M=5.0
A Cooled-Gas Pyrometer for Use in High-Temperature Gas Streams
Cumulative Fatigue Damage at Elevated Temperature
Effect of Advance Ratio on Flight Performance of a Modified Supersonic Propeller
Effect of Precipitate Particles on Creep of Aluminum-Copper Alloys During Age Hardening
Effect of pressure and duct geometry on bluff-body flame stabilization
Effect of Some External Crosswise Stiffeners on the Heat Transfer and Pressure Distribution on a Flat Plate at Mach Numbers of 0.77, 1.39, and 1.98
Effects of compressibility on rotor hovering performance and synthesized blade-section characteristics derived from measured rotor performance of blades having NACA 0015 airfoil tip sections
Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations
Effects of ground proximity on the thrust of a simple downward-directed jet beneath a flat surface
Effects of nose angle and Mach number on transition on cones at supersonic speeds
Effects of Propeller Position and Overlap on the Slipstream Deflection Characteristics of a Wing-Propeller Configuration Equipped With a Sliding and Fowler Flap
Experimental Evaluation of Low-Band-Pass Landing-Gear Shock Absorber for Pulse Loadings
Experimental investigation of axial and normal force characteristics of skewed nozzles
An experimental investigation of the effect of various parameters including tip Mach number on the flutter of some model helicopter rotor blades
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