Call Number (LC) | Title | Results |
---|---|---|
301-Ae8 4: |
Reports and memoranda / Structures of minimum weight / Electronics applied to the measurement of physical quantities / Wind-tunnel flutter tests on a model delta wing under fixed and free root conditions / An approximation simplifying wing flutter calculations / |
6 |
301-Ae8 4:1844 | Flight tests on wing sections using the parasol monoplane / | 1 |
301-Ae8 4:1849 | A graphical method of calculating the performance of an airscrew. | 1 |
301-Ae8 4:1861 | The effect of ground interference on the trim of a low wing monoplane / | 1 |
301-Ae8 4:1865 | Wind tunnel corrections on ground effect / | 1 |
301-Ae8 4:1866 | The use of a freely rotating windmill to improve the flow in a wind tunnel / | 1 |
301-Ae8 4:1867 | The effect of a gauze on the velocity distribution in a uniform duct / | 1 |
301-Ae8 4:1872 | On the power input required to maintain forced oscillations of an aeroplane wing in flight / | 1 |
301-Ae8 4:1902 | Steady two-dimensional flow past a solid cylinder in a non-uniform stream, and, Two-dimensional wind-tunnel interference / | 1 |
301-Ae8 4:1904 | The representation of aircraft wings, tails, and fuselages by semi-rigid structure in dynamic and static problems / | 1 |
301-Ae8 4:1905 | A simple method of constructing stability diagrams / | 1 |
301-Ae8 4:1906 | A philosophy of aeroplane strength factors / | 1 |
301-Ae8 4:1907 | The renewal of aircraft / | 1 |
301-Ae8 4:1908 | On the stressing of polygonal tubes with particular reference to the torsion of tapered tubes of trapezoidal section / | 1 |
301-Ae8 4:1910 | The calculation of aerodynamic loading on surfaces of any shape / | 1 |
301-Ae8 4:1911 | Wood stringer sandwich construction. | 1 |
301-Ae8 4:1912 | Wind tunnel interference effect on the values of experimentally determined derivative coefficients for oscillating aerofoils / | 1 |
301-Ae8 4:1914 | A method for the rapid evaluation of Glauert's expressions for the angle of zero lift and the moment at zero lift / | 1 |
301-Ae8 4:1915 | The response of an aeroplane to the application of ailerons and rudders. | 1 |
301-Ae8 4:1916 | Rational stressing cases for symmetric flight / | 1 |