1998
DOI: 10.1006/icar.1998.5945
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Jetting in Oblique, Asymmetric Impacts

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Cited by 15 publications
(17 citation statements)
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“…The pressure gradient is in the direction to change the deflection angles to those predicted in the free-slip assumption. In reality, the boundary may not strictly follow either boundary condition but may undergo oscillation as observed in explosive welding experiments [e.g., El-Sobky, 1983], analytical calculations [e.g., Godunov et al, 1970], and numerical simulations [Miller, 1998]. Nevertheless, impact experiments of asymmetric collisions using cone-shaped projectiles and flat targets by Allen et al [1959] show that the critical condition is predicted well by the asymmetric collision model with the freeslip boundary condition assumed by Walsh et al [1953].…”
Section: Asymmetric Jettingmentioning
confidence: 99%
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“…The pressure gradient is in the direction to change the deflection angles to those predicted in the free-slip assumption. In reality, the boundary may not strictly follow either boundary condition but may undergo oscillation as observed in explosive welding experiments [e.g., El-Sobky, 1983], analytical calculations [e.g., Godunov et al, 1970], and numerical simulations [Miller, 1998]. Nevertheless, impact experiments of asymmetric collisions using cone-shaped projectiles and flat targets by Allen et al [1959] show that the critical condition is predicted well by the asymmetric collision model with the freeslip boundary condition assumed by Walsh et al [1953].…”
Section: Asymmetric Jettingmentioning
confidence: 99%
“…Because adiabatic compression does not contribute to an increase in thermal energy, the contrast in degree of heating in Figure 13 would be increased further when the effect of coincidence of stagnation pressure is taken into account. Consequently, uncertainty in the method by Kieffer [1977] [Miller, 1998]. Because such oscillatory motion of the material boundary gives rise to motion of shock fronts around the collision point, the effective impact velocity of incoming flow with respect to the shock front will also fluctuate.…”
Section: Model Reassessmentmentioning
confidence: 99%
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“…The emission velocities of a large part of these fragments are low, consequently they will acquire orbits "similar" to Iapetus' and they might impact Iapetus again. Neverthless, we expect a high velocity ricochet for very grazing impacts (see Miller 1998). TYPE2 impacts at β g = 15…”
Section: Remarks and Conclusionmentioning
confidence: 95%
“…This latter case, for example, may be due to a slight focusing of the ejecta or the creation of collimated jets due to a strongly non-central collision (see Martelli et al 1993;Miller 1998). The fragments able to reach Iapetus are those ejected towards Hyperion's motion direction.…”
Section: Transfer Of Massmentioning
confidence: 99%