Tests were conducted on internal wings of Fokker F-27 prototype; loads applied and their sequence were based on strain gage measurements on aircraft flying in turbulent air; tests with random load sequence as well as with programmed load sequence, were carried out, both with and without ground-to-air cycles; test setup and principal results are discussed.
Fatigue tests on large aircraft structures with random load sequence
Vermoeiingsproeven op grote vliegtuigconstructies met willekeurige belastingsvolgorde
Ingenieur ; 77 , n 40
1965
Article (Journal)
Dutch
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