C. Svoboda's Aluminum structural member component weight as a function of PDF

By C. Svoboda

Airplane layout 2 (1999) 231 - 237

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I approached the last machine. My first few shots incapacitated the hostile machine gunner. Possibly they had tickled the pilot, too. At any rate he resolved to land with his bombs. I fired a few more shots to accelerate his progress downwards. He fell close to our flying ground at Lagnicourt. While I was fighting my opponent, Immelmann had tackled another Englishman and had brought him down in the same locality. Both of us flew quickly home in order to have a look at the machines we had downed.

Then I scrambled out to inspect the damage. It was nothing much. A wheel had been broken in the ditch, a steel undercarriage strut twisted. It could all easily be repaired on the spot . . Solicitous inhabitants crowded round, offering help, advice, congratulations, food and drink, shelter for the night, first-aid or a guard for the machine. I asked for a telephone. This was the first time I had broken anything since starting to fly, and now that the anguish of the descent was past I wondered ruefully whether the breaking of a wheel would not put a black mark against my name.

Beneath us there were dense clouds. Voss did not know the country and he began to feel uncomfortable. When we passed above Arras I met my brother who also is in my squadron and who had lost his way. He joined us. Of course he recognized me at once by the color of my machine. Suddenly we saw a squadron approaching from the other side. ” Although there were nine Englishmen and although they were on their own territory they preferred to avoid battle. I thought that perhaps it would be better for me to re-paint my machine.

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Aluminum structural member component weight as a function of wing loading by C. Svoboda

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