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NACA Technical Notes
296
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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
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
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
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
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
Investigation of the compressive strength and creep of 7075-T6 aluminum-alloy plates at elevated temperatures
Stability of elastically supported columns
Analysis of operational airline data to show the effects of airborne weather radar on the gust loads and operating practices of twin-engine short-haul transport airplanes
A relation between burning velocity and quenching distance
Study of Some Burner Cross-Section Changes That Increase Space-Heating Rates
Development of a piston-compressor type light-gas gun for the launching of free-flight models at high velocity
Momentum Transfer for Flow Over a Flat Plate with Blowing
Bending tests of a monocoque box
Abnormal grain growth in M-252 and S-816 alloys
Measurement of Static Pressure on Aircraft
Some Ground Measurements of the Forces Applied by Pilots to a Side-Located Aircraft Controller
Atmospheric temperature observations to 100,000 feet for several climatological regions of the Northern Hemisphere
The Useful Heat Capacity of Several Materials for Ballistic Nose-Cone Construction
Crash Injury
Analysis of elastic thermal stresses in thin plate with spanwise and chordwise variations of temperature and thickness
Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack
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