A wind-tunnel investigation of a B-52 model flutter suppression system

Redd, L. T.; Gilman, Jean; Cooley, D. E.; Sevart, F. D.

doi:10.2514/6.1974-401

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B-52 Model Program1

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1975

2003

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Cited by 5 publications

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“…The aileron loop fed back compensated accelerometer signals from ballasted external fuel tanks while the ap loop fed back compensated accelerometersignalsfrom near the midwing. The wind-tunnel data 26 scaled up to ight conditions compared well with ight-test results. The RC system was designed to reduce the gust-induced vertical acceleration at the pilot's station by at least 30% using the canards commanded by a compensated vertical acceleration sensed at the pilot's station.…”

Section: B-52 Model Programmentioning

confidence: 99%