1. The flow over the Geimini afterbody is separated.

2. The friction drag coefficient increases with increasing afterbody fineness ratio and decreasing Reynolds Number.

3. In the study of civil aircraft afterbody test, it's adopted many kinds of afterbody shape models and the model with or without tail.

4. When the separation distance is small, the region between two stages is filled with "dead water" flow, the bottom drag of forebody is negative, the typical "afterbody effect" phenomenon occurs.

5. The research was made on the afterbody flow field of civil aircraft.

6. The ejecting flying toy also comprises an afterbody form finalizing sheet which is fixed at the center of the rear part of the airfoil.

7. The drag increasing of the larger-upswept afterbody is due to the afterbody separation.

8. A radio frequency electric wire is connected with the afterbody of the radio frequency cutter body and the anterior part of the radio frequency cutter body is provided with a bit.

9. Experiment investigation shows: The main body zero drag can be reduced by faovurable interference of jet flow. Then an optimuns afterbody configuration can be obtained.

10. The method takes into account the effects of a variety of parameters concerning jet, nozzle and afterbody of a missile.

11. The results indicated that three-dimensional open separation exists due to the cross flow around the afterbody, thicker boundary layer and the stronger adverse pressure gradient on the lower surface.

12. At the end of the analysis, it is suggested that exerting the elastic and damping restriction on the afterbody of the headstock was the best reasonable measurement.

13. They are tinned T2 copper which assure the credible conductivity. There is thread in the inner hole of the afterbody of terminals, the insulation covering is hard, there is no break no rebound.

14. Secondly, with the aid of flow visualization and seven-hole probe experiment on the fuselage,[/afterbody.html] the afterbody wake flow was investigated clearly.

15. This paper states a new vibration reduction system of afterbody vibration, called as damp tank.

16. The key problem in the hull form design for a high speed round bilge displacement craft is to select an appropriate afterbody form.

17. There are two shedding modes along the slender axes when the angle of attack is very high. The Karman vortex shedding region is located in afterbody while the nose vortices region is near the apex.