1971
DOI: 10.1016/0022-460x(71)90713-9
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Response of an accelerating vehicle to random road undulation

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Cited by 26 publications
(5 citation statements)
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“…The effect of acceleration on velocity response is more complicated than that found by Yadav and Nigam [4] for acceleration response, but at least it now seems that the lack of effect on displacement response first observed in [3] and confirmed in [t] is an exceptional situation.…”
Section: The Calculation Of E(z 2) Would Thus Involve Such Cross-corrmentioning
confidence: 88%
“…The effect of acceleration on velocity response is more complicated than that found by Yadav and Nigam [4] for acceleration response, but at least it now seems that the lack of effect on displacement response first observed in [3] and confirmed in [t] is an exceptional situation.…”
Section: The Calculation Of E(z 2) Would Thus Involve Such Cross-corrmentioning
confidence: 88%
“…with (•) representing the Fourier transform operator, where ν = ω s /ω s,GC , γ = m u /m s , β = ω u /ω s and ζ = C s /2m s ω s are the quarter-car invariants and κ = νπ + iωζ with i = √ −1. The temporal base excitation process, ξ t (t), in general, is non-stationary and possesses an intime evolutionary spectrum [35][36][37]. However, for the case of constant speedṡ(t) = V, the process becomes stationary with an autocorrelation function that only depends on the time lag τ , that is,…”
Section: Road Vehicle Interaction: a Spectral Stochastic Modelmentioning
confidence: 99%
“…Under this assumption, if the aircraft velocity is constant, the excitation from the rough surface becomes a stationary random process, whereas for the variable aircraft velocity the surface excitation becomes a nonstationary random process. From among the various statistical models of the aircraft landing strip, the most widely used model can be expressed by the equation (Virchis and Robson, 1978) where…”
Section: Modeling the Landing Gear And Landing Strip Surfacementioning
confidence: 99%
“…During take-off and landing, an aircraft landing gear is subjected to random excitations arising from the surface roughness of a landing strip (Yadav and Nigam, 1978 ;Soong and Mircea, 1993 ;Sobczyk et al, 1977 ;Virchis and Robson, 1978). The level of aircraft vibration due to such random excitations needs to be taken into account during structural design not only to guarantee the structural integrity but also to protect the cargo and on-board instrumentation.…”
Section: Introductionmentioning
confidence: 99%