A flight investigation of the effect of mass distribution and control setting on the spinning of the XN2Y-1 airplane (1935)
NASA Technical Reports Server (NTRS) · leaf 1
elocity, ± 3 tests the accelerometer was housed in an insulated box percent for each component; acceleration, ±0.05 g; that was held at a constant temperature by a thermo- interval of altitude, ±3 percent; time, ±3 percent; statically controlled electric heater. Control of the weight, ± 1 percent;… … r. /6%e" s. SJZ" a 3.03' '•26x5 Tire a. Ballast containers, a Clark Y 15% thick, e. Base line. m. £ Hinge. Fiooke 1.—Line drawing and general dimensions of the XN2Y-1 airplane. for frequent changes of the damping oil with changes RESULTS of air temperature. Special precautions were also Before…
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