Comparison of transonic airfoil characteristics by Navier-Stokes computation and by wind tunnel test at high Reynolds number
By: Naoki Hirose, Nobuhiro Kawai and Jun-ichi Miyakawa.
Contributors: Kawai, Nobuhiro.; Miyakawa, Jun-ichi.; National Aerospace Laboratory (Japan)
Publisher: National Aerospace Laboratory
Published: 1986
Place of publication: Tokyo
Number of pages: 15
Subjects: Navier-Stokes equation; Transonic flow
Notes: Bibliographical references: p.14-15.