@article{oai:jaxa.repo.nii.ac.jp:00034381,
 author = {KARASHIMA, Keiichi},
 issue = {1},
 journal = {ISAS report/Institute of Space and Aeronautical Science,University of Tokyo},
 month = {Feb},
 note = {An analytical method for axially symmetric supersonic flow involving shock wave is presented and applied to clarify the characteristic feature of the flow near the region of vertex of the pointed bodies of revolution with arbitrary geometry. The method used in the present approach is exact except for an assumption that the flow is inviscid. It is shown that the present method can be further applied, with a slight modification, to a circular-cone with such large semi-vertex angle that the flow behind the shock wave is partially subsonic. Detailed examination reveals that in axially symmetric flow there exists a particular point which corresponds to Crocco point in plane flow and the flow characters near the region of vertex of the body are qualitatively quite the same as those of the plane flow. It is concluded that the transition from attached to detached shock wave is continuous for circular-cones as well as for plane wedges., 資料番号: SA2400513000},
 pages = {1--30},
 title = {The Flow Near the Region of Vertex of Axially Symmetric Bodies at Supersonic Speeds},
 volume = {31},
 year = {1966}
}