E. Torenbeek's Aircraft design education in Europe PDF

By E. Torenbeek

Plane layout three (2000) 205 - 206

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WARBIRDTECH - based on telemetry that indicated no abrupt motions in pitch, roll, yaw, or acceleration. The board also ruled out the theory that airflow effects from the XB-70A somehow sucked the fighter into the bomber. The finding was that vortices contributed to the collision only after the F-I04 was so close that collision was imminent. The board determined that there were no equipment problems with the XB-70A, and that there were no indications of malfunction on the F-I04N, although the aircraft did not carry telemetry transmitters or recorders so there was no way to know for sure.

4 engine have been installed. (Gerald H. Balzer Collection) A/V-2 under construction. Note the drag chute compartment with one of the two doors installed. Plywood covers most of the upper wing area to prevent damage from people walking on the stainless steel honeycomb skin. The rudders have been installed and their white paint contrasts with the bare metal of the fixed portion of the vertical stabilizer. (Tony Landis Collection) NORTH AMERICAN IB-1~A VA1KIm~ 31 The dry weight of the XB-70A airframe was approximately 150,000 pounds, a little more than a fullyloaded Blackbird.

Of course, the Valkyrie had no onboard toolkit - that would have made things too simple. But Cotton had brought along his briefcase with his various notes and plans, and opening itt he found a binder-type paperclip. Straightening out the paperclip, then grasping the middle of it with a leather glove, Cotton carefully reached in and short circuited the breaker. It did the trick. However, the malfunction also caused hydraulic pressure to remain on three of the four main wheel brakes, which were thus locked when the aircraft landed at 173 knots.

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Aircraft design education in Europe by E. Torenbeek

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