Sentence examples for shock angle from inspiring English sources

While the first orbit represents a crossing of the quasiparallel shock (angle between the shock normal and the upstream magnetic field 30.5 deg), the second one represents a crossing of the quasi-perpendicular shock (angle 75.7 deg).

Oblique shock conditions were imposed for a shock angle of θ= 32.58∘ and Mach 2 free-stream, impinging on a laminar flat-plate boundary-layer.

The numerical results for pitch, track angle, Mach stem angle, and incident shock angle on the tube wall agree well with the experimental results.

The near-nozzle shock structure, the geometry of the Mach disk and reflected shock angle, as well as the turbulent shear layer were all captured in very good agreement with data available in the literature.

The asymmetric nature of the magnetic field disturbance is analogous to that of the TCVs associated with IMF discontinuities (Zesta and Sibeck 2004), and our interpretation of the shock angle effects is consistent with their idea of the discontinuity angle.

We noticed a difference in the shock normal orientation relative to the Sun Earth line based on the shock arrival timing at WIND and ACE, and the role of the shock angle is discussed in "Shock orientation" section.

These authors concluded that the shock impact angle plays a major role in effectively compressing the magnetosphere, thereby leading to a more favorable scenario for cavity mode excitation due to symmetric magnetosphere compression.

Since the IP shock discussed here has very similar properties to the one simulated by Oliveira and Raeder (2014), with exactly the same shock impact angle, their conclusions support the argument of the lack of cavity mode excitation in observed in the event discussed in this paper.

Vaporization of carbonate targets by hypervelocity impact increases with decreasing impact angle (from the horizontal), in contrast with expectations based only on peak shock pressures.

For the multi-compression inlets, the solution strategy of shock wave angle for the leasttotal pressure loss is designed.

However, the SYM-H rise time in our events does not show a clear dependence on the shock normal angle (Table 1).