@article{oai:jaxa.repo.nii.ac.jp:00034386,
 author = {KARASHIMA, Keiichi and IWASAKI, Kenjiro},
 issue = {6},
 journal = {ISAS report/Institute of Space and Aeronautical Science,University of Tokyo},
 month = {Aug},
 note = {A general method of theoretical approach to supersonic flow past lifting bodies of revolution with arbitrary geometry is presented assuming that the flow behind an attached shock wave consists of a basic non-lifting field upon which is superimposed a perturbation field due to small angles of attack and is particularly applied to circularcones as a simple example. It is shown that, although the nonlinearity in fundamental equations predicting the basic field has a predominant effect on aerodynamic characteristics of the body, a linear approximation of perturbation field with respect to angle of attack still seems to be available even if the body is not so slender. Experimental results also confirm this., 資料番号: SA2400529000},
 pages = {117--141},
 title = {Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack},
 volume = {31},
 year = {1966}
}