@article{oai:jaxa.repo.nii.ac.jp:00031177,
 author = {NANBU, Kenichi},
 journal = {The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Symposium on Mechanics for Space Flight},
 month = {Mar},
 note = {By use of the direct-simulation method of Nanbu, the Couette flow for wall Mach number 3 is analysed over the whole range of the Knudsen number. Gas is a monatomic one of Maxwell molecules. By comparing the numerical solution obtained from simulation calculations with the approximate six-moment solution of Liu and Lees, the accuracy of the latter is examined in detail. As to the flow velocity and shearing stress, the six-moment solution shows reasonable agreement with the simulation solution. As to the temperature, density, and heat flux, the error of the six-moment solution is not small in all flow regimes except near-continuum one. As to the pressure, it is not uniform in the transition regime, differently from the prediction of the six-moment solution., 資料番号: SA0033410000},
 pages = {123--139},
 title = {Couette Flow in Continuum to Free Molecular Regime},
 volume = {1},
 year = {1983}
}