Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:6/2009 | Theoretical calculations of the supersonic pressure distribution and wave drag for a limited family of tapered sweptback wings with symmetrical parabolic-arc sections at zero lift / | 1 |
Y 3.N 21/5:6/2010 | Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces / | 1 |
Y 3.N 21/5:6/2011 | Spanwise loading for wings and control surfaces of low aspect ratio / | 1 |
Y 3.N 21/5:6/2012 | Results of shear fatigue tests of joints with 3/16-inch-diameter 24S-T31 rivets in 0.064-inch-thick Alclad sheet / | 1 |
Y 3.N 21/5:6/2013 | A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results / | 1 |
Y 3.N 21/5:6/2014 | Static longitudinal stability and control of a convertible-type airplane as affected by articulated- and rigid-propeller operation / | 1 |
Y 3.N 21/5:6/2015 | Water landing investigation of a model having a heavy beam loading and a 30 degree angle of dead rise / | 1 |
Y 3.N 21/5:6/2016 | Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes / | 1 |
Y 3.N 21/5:6/2017 | A small-deflection theory for curved sandwich plates / | 1 |
Y 3.N 21/5:6/2018 | Low-speed investigation of a thin, faired, double-wedge airfoil section with nose flaps of various chords / | 1 |
Y 3.N 21/5:6/2019 | Penetration of air jets issuing from circular, square, and elliptical orifices directed perpendicularly to an air stream / | 1 |
Y 3.N 21/5:6/2020 | Compressive strength of flanges / | 1 |
Y 3.N 21/5:6/2021 |
Buckling of thin-walled cylinder under axial compression and internal pressure Buckling of thin-walled cylinder under axial compression and internal pressure / |
2 |
Y 3.N 21/5:6/2022 | Propeller flight investigation to determine the effects of blade loading / | 1 |
Y 3.N 21/5:6/2023 | Determination of the rate of roll of pilotless aircraft research models by means of polarized radio waves / | 1 |
Y 3.N 21/5:6/2024 | Sound measurements for five shrouded propellers at static conditions / | 1 |
Y 3.N 21/5:6/2025 | Effect of valve overlap and compression ratio on variation of measured performance with exhaust pressure of aircraft cylinder and on computed performance of compound power plant / | 1 |
Y 3.N 21/5:6/2026 | Tables for determining reduction of energy and intensity of x-rays and gamma-rays at various scattering angles in small thicknesses of matter / | 1 |
Y 3.N 21/5:6/2027 | Friction and wear of hot-pressed bearing materials containing molybdenum disulfide / | 1 |
Y 3.N 21/5:6/2028 | Effect of tunnel configuration and testing technique on cascade performance / | 1 |