@techreport{oai:jaxa.repo.nii.ac.jp:00045029,
 author = {中橋, 和博 and 宮島, 博 and 木皿, 且人 and 毛呂, 明夫 and NAKAHASHI, Kazuhiro and MIYAJIMA, Hiroshi and KISARA, Katsuto and MORO, Akio},
 month = {Jul},
 note = {This report describes numerical schemes used in the computer program for nozzle performance predications of liquid rocket engines. The program is a set consisting of the following four programs: a program of one-dimensional equilibrium flow(ODE), a one-dimensional kinetic flow(ODK), a two-dimensional kinetic flow(TDK), and a turbulent boundary layer(TBL). Published programs were utilized for ODE and TBL, but the programs for ODK and TDK were newly developed. In the TDK program, an efficient numerical scheme for a two-dimensional nonequilibrium flow was devised for rocket nozzle flowfields, and is described in detail in this report. Computational results are presented for hydrogen/oxygen and NTO/A-50 propellant engines, showing the utility of the present computer program by comparing it with available experimental data., 資料番号: NALTR0771000, レポート番号: NAL TR-771},
 title = {ロケットノズルの性能予測計算法},
 year = {1983}
}