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NACA Technical Notes
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NACA Technical Notes
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Technical note (United States. National Advisory Committee for Aeronautics)
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Bending Tests of Metal Monocoque Fuselage Construction
Corrugated Metal Diaphragms for Aircraft Pressure-Measuring Instruments
A preliminary study of a propeller powered by gas jets issuing from the blade tips
Performance of Hoods for Aircraft Exhaust-Gas Turbines
Friction Coefficients in the Inlet Length of Smooth Round Tubes
Tests on Duralumin Columns for Aircraft Construction
On possible similarity solutions for three-dimensional incompressible laminar boundary layers 2: similarity with respect to stationary polar coordinates
Stability Limits and Burning Velocities of Laminar Hydrogen-Air Flames at Reduced Pressure
A velocity-correction formula for the calculation of transonic Mach number distributions over diamond-shaped airfoils
Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61
Heat Capacity Lag in Gases
Experimental Investigation at Low Speed of the Effects of Wing Position on the Static Stability of Models Having Fuselages of Various Cross Section and Unswept and 45 Degrees Sweptback Surfaces
Langley full-scale-tunnel investigations of the maximum-lift and stalling characteristics of a trapezoidal wing of aspect ratio 4 with circular-arc airfoil sections
Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections
Studies on Von Kármán's Similarity Theory and Its Extension to Compressible Flows: A Critical Examination of Similarity Theory for Incompressible Flows
Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flows: A Similarity Theory for Turbulent Boundary Layer Over a Flat Plate in Compressible Flow
Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flow: Investigation of Turbulent Boundary Layer Over a Flat Plate in Compressible Flow by the Similarity Theory
Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and supersonic speeds
Application of Variational Methods to Transonic Flows With Shock Waves
Hydrodynamic Investigation of a Series of Hull Models Suitable for Small Flying Boats and Amphibians
Application of Response Function to Calculation of Flutter Characteristics of a Wing Carrying Concentrated Masses
Investigation of deflectors as gust alleviators on a 0.09-scale model of the Bell X-5 airplane with various wing sweep angles from 20 degrees to 60 degrees at Mach numbers from 0.40 to 0.90
Flight measurements of drag and base pressure of a fin-stabilized parabolic body of revolution (NACA RM-10) at different Reynolds numbers and at Mach numbers from 0.9 to 3.3
Viscosity Corrections to Cone Probes on Rarefied Supersonic Flow at a Nominal Mach Number of 4
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